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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Iframe URL

https://www.satcat.com/sats-embedded/20962?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

20962, 1975-100F

Orbit

GEO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Aerojet

Mission

Spacecraft

Bus & Motor

SVM, SVM-5

Mass

Wet unknown, 31 kg dry

Launch date (UTC)

1975-10-16 (50 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)

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Last TLE update: 2 days ago

TLE from 2 days ago

0 GOES 1 AKM
1 20962U 75100F   25240.25092207  .00000027  00000-0  00000-0 0  9991
2 20962   3.0413 260.5969 0269834  79.6580 283.0869  1.01931715133164

Epoch: 2025-08-28T06:01Z

TLE epoch observation values (Epoch: 2025-08-28T06:01:19.666Z)

Latitude

0.00001°

Longitude

-166.74705°

Altitude

35,099.715 km

Speed

3.108 km/s

True Right ascension

17h 21m 12s

True Declination

0° 00' 00"

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

18:00:51

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

36,454.052 km

Perigee altitude

34,203.27 km

Semi-major axis

41,706.798 km

Eccentricity

0.02698

Inclination

3.0413°

RAAN

260.5969°

Arg. of periapsis

79.658°

True anomaly

280.05339°

Mean anomaly

283.0869°

Eccentric anomaly

281.57229°

Mean motion

0.25482 °/min

Orbital period

1,412.76 mins

BSTAR

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Computing Atmospheric mass density...

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Other satellites on launch #100 in the year 1975 (1975-10-16 UTC)

GOES 1 (SMS-C), 8366

DELTA 1 R/B(1), 8367 (Decayed)

DELTA 1 R/B(2), 8368 (Decayed)

DELTA 1 DEB, 8371 (Decayed)

DELTA 1 DEB, 8372 (Decayed)

GOES 1 AKM Visibility forecast

Observer location: undefined°, undefined°
Set Observer location

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.
1440 mins	2025-08-30 02:27:10.423Z	240.377° WSW	2025-08-30 13:57:10.423Z	235.945° WSW	25.471°	2025-08-31 02:27:10.423Z	235.494° WSW

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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

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Check out GOES 1 AKM, 20962 on other resources

View GOES 1 AKM, 20962 on Heavens-Above

View GOES 1 AKM, 20962 on Keep Track

View GOES 1 AKM, 20962 on Celestrak

View GOES 1 AKM, 20962 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

GOES 1 AKM, 20962

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2025-08-28T06:01:19.666Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #100 in the year 1975 (1975-10-16 UTC)

GOES 1 AKM Visibility forecast

20962 neighbors

Co-orbital & Co-planar RSOs

Check out GOES 1 AKM, 20962 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago