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.
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20799 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Aerojet
Mission
Spacecraft
Bus & Motor
SVM, SVM-5
Mass
Wet unknown, 31 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GOES 2 AKM
1 20799U 77048G 25306.34489284 -.00000383 00000-0 00000+0 0 9995
2 20799 4.6822 278.3625 0205411 101.0992 261.0292 1.00574462115546Epoch: 2025-11-02T08:16Z
TLE epoch observation values (Epoch: 2025-11-02T08:16:38.741Z)
Latitude
-0.00216°
Longitude
112.10123°
Altitude
35,856.937 km
Speed
3.066 km/s
True Right ascension
18h 32m 29s
True Declination
0° 00' 08"
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
14:13:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,567.412 km
Perigee altitude
34,838.626 km
Semi-major axis
42,081.156 km
Eccentricity
0.02054
Inclination
4.6822°
RAAN
278.3625°
Arg. of periapsis
101.0992°
True anomaly
258.71406°
Mean anomaly
261.0292°
Eccentric anomaly
259.87063°
Mean motion
0.25143 °/min
Orbital period
1,431.83 mins
BSTAR
0
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Other satellites on launch #48 in the year 1977 (1977-06-16 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 2 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 2 AKM is likely not visible in the next few days. |
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20799 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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