Showing default

TOPEX/POSEIDON, 22076

Orbit data source: Space-Track

TOPEX/POSEIDON, 22076 is an American payload satellite 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.

Loading next visibility...
Identifier
22076, 1992-052A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Fairchild
Mission
Non-operational Civil Science
Bus & Motor
MMS, Unknown motor
Mass
2,402 kg wet, 2,185 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 + 1 Pan, 5.8 m
Radar Cross Section
20.954 m², Large (>1 m²)

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

TLE from 17 hours ago
0 TOPEX/POSEIDON
1 22076U 92052A   25260.23526245 -.00000049  00000-0  54013-4 0  9990
2 22076  66.0440 339.2676 0007793 270.4065 113.9526 12.81084630548529
Epoch: 2025-09-17T05:38Z
TLE epoch observation values (Epoch: 2025-09-17T05:38:46.675Z)
Latitude
22.24549°
Longitude
-91.42314°
Altitude
1,341.291 km
Speed
7.188 km/s
True Right ascension
23h 18m 44s
True Declination
22° 08' 04"
Sunlit
Object was in full shadow 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
15:38:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,341.686 km
Perigee altitude
1,329.663 km
Semi-major axis
7,713.812 km
Eccentricity
0.00078
Inclination
66.044°
RAAN
339.2676°
Arg. of periapsis
270.4065°
True anomaly
114.03418°
Mean anomaly
113.9526°
Eccentric anomaly
113.99339°
Mean motion
3.20361 °/min
Orbital period
112.37 mins
BSTAR
0.000054013
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|