GOES 1 AKM, 20962

Orbit data source: Space-Track

GOES 1 AKM, 20962 is space debris in GEO originally from a launch on Thu, 16 Oct 1975 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

Not visible in the next 10 days
Identifier
20962, 1975-100F
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
Aerojet
Mission
Spacecraft
Bus & Motor
SVM, SVM-5
Mass
Wet unknown, 31 kg dry
Launch date (UTC)
1975-10-16 (50 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 GOES 1 AKM
1 20962U 75100F   26089.09579972 -.00000058  00000-0  00000+0 0  9998
2 20962   2.5043 254.5485 0271427  90.3263 272.1985  1.01933060135347
Epoch: 2026-03-30T02:17Z
TLE epoch observation values (Epoch: 2026-03-30T02:17:57.095Z)
Latitude
-0°
Longitude
31.99325°
Altitude
35,316.465 km
Speed
3.092 km/s
True Right ascension
16h 55m 53s
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
11:16:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,460.321 km
Perigee altitude
34,196.27 km
Semi-major axis
41,706.433 km
Eccentricity
0.02714
Inclination
2.5043°
RAAN
254.5485°
Arg. of periapsis
90.3263°
True anomaly
269.08794°
Mean anomaly
272.1985°
Eccentric anomaly
270.64344°
Mean motion
0.25482 °/min
Orbital period
1,412.75 mins
BSTAR
0
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