Key statistics
Satellite S80/T at a glance.
Uptime
12020
Days in orbit
Revolutions
≈ 12.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
66.1
Latest
Satellite identification and parameters
Extended collection of information and parameters for S80/T.
Object identification
Identified? True
Debris? False
Object name: S80/T
International designator: 1992-052C
Object number (NORAD): 22078
Object ID (CCSDS): 22078
Country: FRANCE (FR)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 111.902 minutes
Inclination: 66.085 deg
SMA: 7692.216 km
Apoapsis: 1315.197 km
Periapsis: 1312.965 km
RAAN: 270.8649 deg
Eccentricy: 0.0001451
Argument of periapsis: 86.1168 deg
Mean anomaly: 274.0017 deg
Mean motion: 12.86842886 rev/day
Mean motion (dot): -0.00000042 rev/day2
B* drag term: 0.000080281 1/REarth
Two-line elements (TLE)
Creation date: July 7, 2025, 6:34 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, noon UTC
TLE line 0: 0 S80/T
TLE line 1: 1 22078U 92052C 25188.50033700 -.00000042 00000-0 80281-4 0 9999
TLE line 2: 2 22078 66.0850 270.8649 0001451 86.1168 274.0017 12.86842886545887
Live tracking on map
Real-time ground track for satellite S80/T.
In-orbit conjunctions
There are no conjunctions computed for S80/T, at the moment. Check back to stay up to date, as we update our databases every day.
Go to all conjunctionsAssociated space launch
The TOPEX/POSEIDON satellite was launched on 10 August 1992 with the objective of "observing and understanding the ocean circulation". A joint project between NASA, the U.S. space agency, and CNES, the French space agency, it carries two radar altimeters and precise orbit determination systems, including the DORIS system. KITSAT-1 (Korean Institute of Technology Satellite) was a collaborative research mission, encompassing the installation of a groundstation in South Korea, participation of Korean engineers in the UoSAT-5 mission, technology transfer and training of students on the MSc courses at Surrey, and the involvement in a engineering and flight microsatellites. The S80/T satellite was built for CNES by Matra Marconi Space using the Surrey Satellite Technology Microbus (Uosat) bus.
S80/T was lifted into orbit during the mission ‘Ariane 42P | Topex-Poseidon, Kitsat 1 & S80/T’, on board a Ariane 42P space rocket.
The launch took place on Aug. 10, 1992, 11:08 p.m. from Ariane Launch Area 2.
For more information about the launch, click the button.
Ariane 42P | Topex-Poseidon, Kitsat 1 & S80/T
Agency: N/A
Status: Launch Successful
Launch date: Aug. 10, 1992, 11:08 p.m. UTC
Rocket: Ariane 42P
Launch pad: Ariane Launch Area 2
Location: Guiana Space Centre, French Guiana
...
Latest news about this satellite
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