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
CYL, 0.6 m
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 5 AKM
1 33521U 81049D   26251.30894980 -.00000208  00000-0  00000+0 0  9993
2 33521  16.1172 317.1401 1708490 145.7555 282.7130  0.82272875 59280
Epoch: 2026-09-08T07:24Z
TLE epoch observation values (Epoch: 2026-09-08T07:24:53.262Z)
Latitude
12.05151°
Longitude
-93.75042°
Altitude
41,358.98 km
Speed
2.901 km/s
True Right ascension
00h 19m 23s
True Declination
12° 02' 28"
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
00:44:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
49,951.833 km
Perigee altitude
33,512.618 km
Semi-major axis
48,110.363 km
Eccentricity
0.17085
Inclination
16.1172°
RAAN
317.1401°
Arg. of periapsis
145.7555°
True anomaly
263.06931°
Mean anomaly
282.713°
Eccentric anomaly
272.93693°
Mean motion
0.20568 °/min
Orbital period
1,750.32 mins
BSTAR
0
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Other satellites on launch #49 in the year 1981 (1981-05-22 UTC)

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