GOES 2 AKM, 20799

Orbit data source: Space-Track

GOES 2 AKM, 20799 is space debris in GEO originally from a launch on Thu, 16 Jun 1977 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
20799, 1977-048G
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)
1977-06-16 (49 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 4.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

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

TLE from 4 hours ago
0 GOES 2 AKM
1 20799U 77048G   26256.59560722 -.00000383  00000-0  00000-0 0  9995
2 20799   3.8801 274.2369 0208077 112.0148 275.8106  1.00582945118725
Epoch: 2026-09-13T14:17Z
TLE epoch observation values (Epoch: 2026-09-13T14:17:40.463Z)
Latitude
1.68322°
Longitude
92.62834°
Altitude
35,624.018 km
Speed
3.083 km/s
True Right ascension
19h 58m 32s
True Declination
1° 40' 53"
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
11:18:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,576.219 km
Perigee altitude
34,825.094 km
Semi-major axis
42,078.793 km
Eccentricity
0.02081
Inclination
3.8801°
RAAN
274.2369°
Arg. of periapsis
112.0148°
True anomaly
273.43288°
Mean anomaly
275.8106°
Eccentric anomaly
274.62228°
Mean motion
0.25145 °/min
Orbital period
1,431.71 mins
BSTAR
0
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