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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33521 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 GOES 5 AKM
1 33521U 81049D 25255.14230686 -.00000184 00000-0 00000-0 0 9999
2 33521 16.9654 319.2435 1697416 138.9058 237.1050 0.82272718 56312
Epoch: 2025-09-12T03:24Z
TLE epoch observation values (Epoch: 2025-09-12T03:24:55.312Z)
Latitude
0.45918°
Longitude
-81.8478°
Altitude
47,008.846 km
Speed
2.578 km/s
True Right ascension
21h 23m 06s
True Declination
0° 27' 32"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
15:40:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
49,898.613 km
Perigee altitude
33,565.937 km
Semi-major axis
48,110.412 km
Eccentricity
0.16974
Inclination
16.9654°
RAAN
319.2435°
Arg. of periapsis
138.9058°
True anomaly
222.6191°
Mean anomaly
237.105°
Eccentric anomaly
229.6889°
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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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GOES 5 AKM Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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GOES 5 AKM is likely not visible in the next few days. |
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33521 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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