GOES 1 AKM, 20962
Orbit data source: Space-Track
GOES 1 AKM, 20962 is space debris in GEO originally from a launch on Thu, 16 Oct 1975 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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20962 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GOES 1 AKM
1 20962U 75100F 26089.09579972 -.00000058 00000-0 00000+0 0 9998
2 20962 2.5043 254.5485 0271427 90.3263 272.1985 1.01933060135347Epoch: 2026-03-30T02:17Z
TLE epoch observation values (Epoch: 2026-03-30T02:17:57.095Z)
Latitude
-0°
Longitude
31.99325°
Altitude
35,316.465 km
Speed
3.092 km/s
True Right ascension
16h 55m 53s
True Declination
0° 00' 00"
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
09:50:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,460.321 km
Perigee altitude
34,196.27 km
Semi-major axis
41,706.433 km
Eccentricity
0.02714
Inclination
2.5043°
RAAN
254.5485°
Arg. of periapsis
90.3263°
True anomaly
269.08794°
Mean anomaly
272.1985°
Eccentric anomaly
270.64344°
Mean motion
0.25482 °/min
Orbital period
1,412.75 mins
BSTAR
0
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Other satellites on launch #100 in the year 1975 (1975-10-16 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 1 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 1 AKM is likely not visible in the next few days. |
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20962 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 descending 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 descending order |
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