general navigation structure general satellite info ilrs support retroreflector info center of mass site performance info

Galileo

Jump to: Mission Objectives, Mission Instrumentation, Mission Parameters, Additional Information

Mission Photos:

Galileo Satellite
Courtesy of ESA

Mission Objectives:

Galileo is a satellite radio navigation system initiative launched by the European Union and the European Space Agency. Galileo consists of a constellation of 30 satellites (27 operational satellites plus 3 satellites in reserve) and ground stations providing position information to users in many sectors (transportation, social services, justice system, custom services, public works, search and rescue, etc.). Two experimental spacecraft were launched in 2005 and 2008 as part of the Galileo System Test Bed V2: GIOVE-A (Galileo In-Orbit Validation Element, formerly GSTB-V2/A) and GIOVE-B (formerly GSTB-V2/B).

The main objectives of the Galileo system are:

  • Provide global navigation satellite system specifically for civilian purposes
  • Generate new, large markets and provide the critical advance in technology for Europe and its partners
  • Provide global Search and Rescue (SAR) function

The Galileo system consists of global, regional and local components. The global component consists of the satellites and ground segment. The regional component consist of a number off External Region Integrity Systems (ERIS) implemented to obtain higher integrity services independent of the Galileo system. Local components may be deployed for enhancing the performance of Galileo locally. These will enable higher performance such as the delivery of navigation signal in areas where the satellite signals cannot be received.

All Galileo satellites will be equipped with LLR arrays to provide precise orbit determination. Both routine SLR tracking and occasional campaigns with more intense tracking will be required. Laser tracking of Galileo will be comparable to GLONASS and GPS tracking (perhaps up to 40 percent more return energy than GPS).

Due to a launch anomaly, the first two Fully Operational Capability (FOC) Galileo satellites (-201 and -202), launched August 22, did not reach their expected orbit. A series of maneuvers were used to push the satellites to useable orbits.

Mission Instrumentation:

Galileo will have the following components:

  • Satellite components:
    • L-band antenna for transmitting navigation signals
    • Search and rescue (S&R) antenna to pick up distress signals
    • C-band antenna to receive signals from up-link stations
    • Two S-band antennas for transmiting housekeeping data and receiving control commands
    • IR Earth sensors for spacecraft pointing
    • FSS sun sensors for spacecraft pointing
    • Laser retro-reflector array for orbit determination
    • Space radiators for heat exchange
  • Interior payload:
    • Passive maser clock
    • Rubidium clock
    • Clock monitoring and control unit
    • Navigation signal generator
    • Remote terminal unit
  • Interior service module:
    • Solar array drive mechanism (SADM)
    • Gyroscopes
    • Reaction wheels
    • Magneto bar
    • Power conditioning and distribution unit
    • On-board computer
Mission Parameters:
Galileo-101 Galileo-102 Galileo-103 Galileo-104
Sponsor: ESA ESA ESA ESA
Expected Life: 12 years 12 years 12 years 12 years
Primary Applications: Positioning Positioning Positioning Positioning
COSPAR ID: 1106001 1106002 1205501 1205502
SIC Code: 7101 7102 7103 7104
Satellite Catalog (NORAD) Number: 37846 37847 38857 38858
PRN E11 E12 E19 E20
Launch Date: 21-Oct-2011 21-Oct-2011 12-Oct-2012 12-Oct-2012
RRA Size:        
RRA Shape: planar planar planar planar
Reflectors: 84 corner cubes 84 corner cubes 84 corner cubes 84 corner cubes
Size of Reflector: 33 mm diameter, 23.3 mm height 33 mm diameter, 23.3 mm height 33 mm diameter, 23.3 mm height 33 mm diameter, 23.3 mm height
Orbit: near-circular near-circular near-circular near-circular
Orbital period: 14.08 hrs 14.08 hrs 14.08 hrs 14.08 hrs
Inclination: 56 degrees 56 degrees 56 degrees 56 degrees
Altitude: 23,220 km 23,220 km 23,220 km 23,220 km
Eccentricity: < 0.001 < 0.001 < 0.001 < 0.001

 

Galileo-201 Galileo-202 Galileo-203 Galileo-204
Sponsor: ESA ESA ESA ESA
Expected Life: 12 years 12 years 12 years 12 years
Primary Applications: Positioning Positioning Positioning Positioning
COSPAR ID: 1405001 1405002 1501701 1501702
SIC Code: 7201 7202 7203 7204
Satellite Catalog (NORAD) Number: 40128 40129 40544 40545
PRN E18 E14 E26 E22
Launch Date: 22-Aug-2014 22-Aug-2014 27-Mar-2015 27-Mar-2015
RRA Size:        
RRA Shape: planar planar planar planar
Reflectors: 60 corner cubes 60 corner cubes 60 corner cubes 60 corner cubes
Size of Reflector: 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height
Orbit: eccentric eccentric near-circular near-circular
Orbital period:     14.08 hrs 14.08 hrs
Inclination: 50 degrees 50 degrees 56 degrees 56 degrees
Altitude: 17,000 - 26,210 km 17,000 - 26,210 km 23,220 km 23,220 km
Eccentricity: ~ 0.158 ~ 0.158 < 0.001 < 0.001

 

Galileo-205 Galileo-206 Galileo-207 Galileo-208
Sponsor: ESA ESA ESA ESA
Expected Life: 12 years 12 years 12 years 12 years
Primary Applications: Positioning Positioning Positioning Positioning
COSPAR ID: 1504501 1504502 1606901 1507902
SIC Code: 7205 7206 7207 7208
Satellite Catalog (NORAD) Number: 40889 40890 41859 41175
PRN E24 E30 E07 E08
Launch Date: 11-Sep-2015 11-Sep-2015 17-Nov-2016 17-Dec-2015
RRA Size:        
RRA Shape: planar planar planar planar
Reflectors: 60 corner cubes 60 corner cubes 60 corner cubes 60 corner cubes
Size of Reflector: 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height
Orbit: near-circular near-circular near-circular near-circular
Orbital period:        
Inclination: 56 degrees 56 degrees 56 degrees 56 degrees
Altitude: 23,220 km 23,220 km 23,220 km 23,220 km
Eccentricity: < 0.001 < 0.001 < 0.001 < 0.001

 

Galileo-209 Galileo-210 Galileo-211 Galileo-212
Sponsor: ESA ESA ESA ESA
Expected Life: 12 years 12 years 12 years 12 years
Primary Applications: Positioning Positioning Positioning Positioning
COSPAR ID: 1507901 1603002 1603001 1606902
SIC Code: 7209 7210 7211 7212
Satellite Catalog (NORAD) Number: 41174 41550 41549 41860
PRN E09 E01 E02 E03
Launch Date: 17-Dec-2015 24-May-2016 24-May-2016 17-Nov-2016
RRA Size:        
RRA Shape: planar planar planar planar
Reflectors: 60 corner cubes 60 corner cubes 60 corner cubes 60 corner cubes
Size of Reflector: 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height
Orbit: near-circular near-circular near-circular near-circular
Orbital period:        
Inclination: 56 degrees 56 degrees 56 degrees 56 degrees
Altitude: 23,220 km 23,220 km 23,220 km 23,220 km
Eccentricity: < 0.001 < 0.001 < 0.001 < 0.001

 

Galileo-213 Galileo-214 Galileo-215 Galileo-216
Sponsor: ESA ESA ESA ESA
Expected Life: 12 years 12 years 12 years 12 years
Primary Applications: Positioning Positioning Positioning Positioning
COSPAR ID: 1606903 1606904 1707901 1707902
SIC Code: 7213 7214    
Satellite Catalog (NORAD) Number: 41861 41862 43055 43056
PRN E04 E05 E21 E25
Launch Date: 17-Nov-2016 17-Nov-2016 12-Dec-2017 12-Dec-2017
RRA Size:        
RRA Shape: planar planar planar planar
Reflectors: 60 corner cubes 60 corner cubes 60 corner cubes 60 corner cubes
Size of Reflector: 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height
Orbit: near-circular near-circular near-circular near-circular
Orbital period:        
Inclination: 56 degrees 56 degrees 56 degrees 56 degrees
Altitude: 23,220 km 23,220 km 23,220 km 23,220 km
Eccentricity: < 0.001 < 0.001 < 0.001 < 0.001

 

Galileo-217 Galileo-218 Galileo-219 Galileo-220
Sponsor: ESA ESA ESA ESA
Expected Life: 12 years 12 years 12 years 12 years
Primary Applications: Positioning Positioning Positioning Positioning
COSPAR ID: 1707903 1707904 1806003 1806004
SIC Code: 7217 7218 7219 7220
Satellite Catalog (NORAD) Number: 43057 43058 43566 43567
PRN E27 E31 E36 E13
Launch Date: 12-Dec-2017 12-Dec-2017 25-Jul-2018 25-Jul-2018
RRA Size:        
RRA Shape: planar planar planar planar
Reflectors: 60 corner cubes 60 corner cubes 60 corner cubes 60 corner cubes
Size of Reflector: 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height
Orbit: near-circular near-circular near-circular near-circular
Orbital period:        
Inclination: 56 degrees 56 degrees 56 degrees 56 degrees
Altitude: 23,220 km 23,220 km 23,220 km 23,220 km
Eccentricity: < 0.001 < 0.001 < 0.001 < 0.001

 

Galileo-221 Galileo-222 Galileo-223 Galileo-224
Sponsor: ESA ESA ESA ESA
Expected Life: 12 years 12 years 12 years 12 years
Primary Applications: Positioning Positioning Positioning Positioning
COSPAR ID: 1806001 1806002 2111601 2111602
SIC Code: 7221 7222 7223 7224
Satellite Catalog (NORAD) Number: 43564 43565 49809 49810
PRN E15 E33 E34 E10
Launch Date: 2018-07-25 2018-07-25 2021-12-05 2021-12-05
RRA Size:        
RRA Shape: planar planar planar planar
Reflectors: 60 corner cubes 60 corner cubes 60 corner cubes 60 corner cubes
Size of Reflector: 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height
Orbit: near-circular near-circular near-circular near-circular
Orbital period:        
Inclination: 56 degrees 56 degrees 56 degrees 56 degrees
Altitude: 23,220 km 23,220 km 23,220 km 23,220 km
Eccentricity: < 0.001 < 0.001 < 0.001 < 0.001

 

Galileo-225 Galileo-226 Galileo-227 Galileo-232
Sponsor: ESA ESA ESA ESA
Expected Life: 12 years 12 years 12 years 12 years
Primary Applications: Positioning Positioning Positioning Positioning
COSPAR ID: 2407901 2416702 2407903 2416701
SIC Code: 7225 7226 7227 7232
Satellite Catalog (NORAD) Number: 59598 61183 59600 61182
PRN E29 E23 E06 E16
Launch Date: 2024-04-28 2024-09-17 2024-04-28 2024-09-17
RRA Size:        
RRA Shape: planar planar planar planar
Reflectors: 60 corner cubes 60 corner cubes 60 corner cubes 60 corner cubes
Size of Reflector: 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height 28.2 mm diameter, 19.1 mm height
Orbit: near-circular near-circular near-circular near-circular
Orbital period:   844.7 minutes    844.7 minutes
Inclination: 56 degrees 55.4 degrees 56 degrees 55.4 degrees
Altitude: 23,220 km 23,235.0 km 23,220 km 23,235.0 km
Eccentricity: < 0.001 < 0.001 < 0.001 < 0.001
Additional Information:
Publications:
  • Falcone M., Hahn J., Burger T. (2017). "Galileo". In: Teunissen, P.J., Montenbruck, O. (eds) Springer Handbook of Global Navigation Satellite Systems. Springer Handbooks. Springer, Cham. doi: 10.1007/978-3-319-42928-1_9
  • Bhattarai S., Ziebart M., Springer T. et al. (2022). "High-precision physics-based radiation force models for the Galileo spacecraft", Adv. Space Res., 69(12), 4141–4154, doi: 10.1016/j.asr.2022.04.003
  • Chen G., Guo J., Gent T. and Zhao QL. (2023). "Multi-GNSS orbit combination at Wuhan University: strategy and preliminary products", J. Geodesy, 97(5), doi: 10.1007/s00190-023-01732-2
  • Defraigne P., Pinat E., Petit G., Meynadier F. (2023). "Monitoring the offset between UTC and its prediction broadcast by the GNSS", Metrologia, 60(6), doi: 10.1088/1681-7575/ad0562
  • Dell'Agnello S., Boni A., Cantone C. et al. (2016). "Thermo-optical vacuum testing of Galileo In-orbit Validation laser retroreflectors", Adv. Space Res., 57(11), 2347–2358, doi: 10.1016/j.asr.2016.03.025
  • Delva P., Puchades N., Schönemann E. et al. (2018). "Gravitational redshift test using eccentric Galileo satellites", Phys. Rev. Lett., 121(23), doi: 10.1103/PhysRevLett.121.231101
  • Duan B., Hugentobler U. (2022). "Estimating surface optical properties and thermal thrust for Galileo satellite body and solar panels", GPS Solutions, 26(135), doi: 10.1007/s10291-022-01324-1
  • Gao F., Li XX, Zhang XH, Wang JL (2017). "Assessment of precise orbit and clock products for Galileo, BeiDou, and QZSS from IGS Multi-GNSS Experiment (MGEX)", GPS Solutions, 21(1), 279-250, doi: 10.1007/s10291-016-0523-3
  • Kawate K., Igarashi Y., Yamada H. et al. (2023). "MADOCA: Japanese precise orbit and clock determination for GNSS", Adv. Space Res., 71(10), 3927–3950, doi: 10.1016/j.asr.2023.01.060
  • Montenbruck O., Steigenberger P., Prange L. et al. (2017). "The Multi-GNSS Experiment (MGEX) of the International GNSS Service (IGS) – Achievements, prospects and challenges", Adv. Space Res., 59(7), 1671–1697, doi: 10.1016/j.asr.2017.01.011
  • Prange L., Villager A., Sidorov D. et al. (2020). "Overview of CODE’s MGEX solution with a focus on Galileo", Adv. Space Res., 66(12), 2786–2798, doi: 10.1016/j.asr.2020.04.038
  • Sośnica K., Zajdel R., Bury G. et al. (2020). "Quality assessment of experimental IGS multi-GNSS combined orbits", GPS Solutions, 24(2), doi: 10.1007/s10291-020-0965-5
  • Steigenberger P., Thoelert S., Montenbruck O. (2018). "GNSS satellite transmit power and its impact on orbit determination", J. Geodesy, 92(6), 609–624, doi: 10.1007/s00190-017-1082-2
  • Villager A., Dach R., Schaer S. et al. (2020). "GNSS scale determination using calibrated receiver and Galileo satellite antenna patterns", J. Geodesy, 94(9), doi: 10.1007/s00190-020-01417-0
  • Zajdel R., Masoumi S., Sośnica K. et al. (2023). "Combination and SLR validation of IGS Repro3 orbits for ITRF2020", J. Geodesy, 97(87), doi: 10.1007/s00190-023-01777-3