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S80/T, 22078

Orbit data source: Space-Track

S80/T, 22078 is a payload satellite owned by CNES (FR) in LEO that was launched on Mon, 10 Aug 1992 UTC via an ARIANE 42P launch vehicle from the French Guiana (FRGUI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
22078, 1992-052C
Orbit
LEO
Country
Flag of FRFR
Related business
Manufacturer
SSTL/MMST
Mission
Civil Communications
Bus & Motor
UOSAT, Unknown motor
Mass
50 kg wet, 50 kg dry
Launch date (UTC)
1992-08-10 (33 years ago)
Launch vehicle
ARIANE 42P
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Hex Poly, 0.3 m
Radar Cross Section
0.140 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 S80/T
1 22078U 92052C   25260.23344907 -.00000052  00000-0  39234-4 0  9997
2 22078  66.0832 120.5252 0005121 359.6929   0.4085 12.86843394555117
Epoch: 2025-09-17T05:36Z
TLE epoch observation values (Epoch: 2025-09-17T05:36:09.999Z)
Latitude
-0.00009°
Longitude
40.07116°
Altitude
1,312.057 km
Speed
7.203 km/s
True Right ascension
08h 02m 06s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
15:41:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,316.569 km
Perigee altitude
1,308.693 km
Semi-major axis
7,690.768 km
Eccentricity
0.00051
Inclination
66.0832°
RAAN
120.5252°
Arg. of periapsis
359.6929°
True anomaly
0.40892°
Mean anomaly
0.4085°
Eccentric anomaly
0.40871°
Mean motion
3.21802 °/min
Orbital period
111.87 mins
BSTAR
0.000039234
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