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 (34 years ago)
Launch vehicle
ARIANE 42P
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Hex Poly + 1 Pan, 6.8 m
Radar Cross Section
20.954 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 hours ago

TLE from 4 hours ago
0 TOPEX/POSEIDON
1 22076U 92052A   26139.53610440 -.00000046  00000-0  66702-4 0  9995
2 22076  66.0397 191.6948 0008299 270.5653 259.7060 12.81093178579813
Epoch: 2026-05-19T12:51Z
TLE epoch observation values (Epoch: 2026-05-19T12:51:59.420Z)
Latitude
8.92644°
Longitude
-62.49399°
Altitude
1,339.426 km
Speed
7.189 km/s
True Right ascension
00h 30m 50s
True Declination
8° 52' 40"
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
01:22:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,342.042 km
Perigee altitude
1,329.239 km
Semi-major axis
7,713.778 km
Eccentricity
0.00083
Inclination
66.0397°
RAAN
191.6948°
Arg. of periapsis
270.5653°
True anomaly
259.61245°
Mean anomaly
259.706°
Eccentric anomaly
259.65922°
Mean motion
3.20363 °/min
Orbital period
112.37 mins
BSTAR
0.000066702
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
|