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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 (34 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: 10 hours ago

TLE from 10 hours ago
0 S80/T
1 22078U 92052C   26319.33434145 -.00000059  00000-0  11745-4 0  9992
2 22078  66.0855 311.6605 0015535 241.8519 118.0930 12.86856056609680
Epoch: 2026-11-15T08:01Z
TLE epoch observation values (Epoch: 2026-11-15T08:01:27.101Z)
Latitude
-0.00005°
Longitude
136.87129°
Altitude
1,321.588 km
Speed
7.194 km/s
True Right ascension
20h 46m 38s
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
15:08:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,324.528 km
Perigee altitude
1,300.633 km
Semi-major axis
7,690.717 km
Eccentricity
0.00155
Inclination
66.0855°
RAAN
311.6605°
Arg. of periapsis
241.8519°
True anomaly
118.2499°
Mean anomaly
118.093°
Eccentric anomaly
118.17146°
Mean motion
3.21805 °/min
Orbital period
111.87 mins
BSTAR
0.000011745
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