GOES 5 AKM, 33521

Orbit data source: Space-Track

GOES 5 AKM, 33521 is space debris in GEO originally from a launch on Fri, 22 May 1981 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.

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Identifier
33521, 1981-049D
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 27, Unknown motor
Mass
Wet unknown, ~50 kg dry
Launch date (UTC)
1981-05-22 (45 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: 15 hours ago

TLE from 15 hours ago
0 GOES 5 AKM
1 33521U 81049D   25348.76652310 -.00000237  00000-0  00000-0 0  9991
2 33521  16.7441 318.6955 1698667 140.6763 245.4559  0.82272370 57081
Epoch: 2025-12-14T18:23Z
TLE epoch observation values (Epoch: 2025-12-14T18:23:47.595Z)
Latitude
2.87785°
Longitude
-31.36994°
Altitude
46,142.033 km
Speed
2.626 km/s
True Right ascension
21h 53m 00s
True Declination
2° 52' 32"
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
08:23:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
49,904.794 km
Perigee altitude
33,560.033 km
Semi-major axis
48,110.551 km
Eccentricity
0.16987
Inclination
16.7441°
RAAN
318.6955°
Arg. of periapsis
140.6763°
True anomaly
229.39852°
Mean anomaly
245.4559°
Eccentric anomaly
237.26865°
Mean motion
0.20568 °/min
Orbital period
1,750.33 mins
BSTAR
0
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Other satellites on launch #49 in the year 1981 (1981-05-22 UTC)

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