NIMBUS 6, 7924
Orbit data source: Space-Track
NIMBUS 6, 7924 is a payload satellite owned by GSFC (US) in SSO that was launched on Thu, 12 Jun 1975 UTC via a DELTA 2910 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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7924 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
GE/MSVD
Mission
Non-operational spacecraft
Bus & Motor
NIMBUS, Unknown motor
Mass
827 kg wet, 827 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
CONE + 2 PAN, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 NIMBUS 6
1 07924U 75052A 26301.68705527 -.00000015 00000-0 53512-4 0 9990
2 07924 99.9957 212.2437 0007167 260.2574 166.1663 13.40827382514029Epoch: 2026-10-28T16:29Z
TLE epoch observation values (Epoch: 2026-10-28T16:29:21.575Z)
Latitude
64.60927°
Longitude
-93.80948°
Altitude
1,122.457 km
Speed
7.295 km/s
True Right ascension
12h 42m 15s
True Declination
64° 28' 56"
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
14:51:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,108.89 km
Perigee altitude
1,098.166 km
Semi-major axis
7,481.665 km
Eccentricity
0.00072
Inclination
99.9957°
RAAN
212.2437°
Arg. of periapsis
260.2574°
True anomaly
166.18592°
Mean anomaly
166.1663°
Eccentric anomaly
166.17611°
Mean motion
3.35387 °/min
Orbital period
107.34 mins
BSTAR
0.000053512
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Other satellites on launch #52 in the year 1975 (1975-06-12 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.NIMBUS 6 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-10-30 06:22:26.672Z | 31.554° NE | 2026-10-30 06:28:26.672Z | 104.016° ESE | 41.373° | 2026-10-30 06:34:26.672Z | 167.9° S |
| 10 mins | 2026-10-30 08:09:26.672Z | 350.485° N | 2026-10-30 08:13:26.672Z | 303.49° NW | 34.873° | 2026-10-30 08:19:26.672Z | 234.991° WSW |
| 8 mins | 2026-10-30 16:41:26.672Z | 96.437° ESE | 2026-10-30 16:44:26.672Z | 62.639° ENE | 24.048° | 2026-10-30 16:49:26.672Z | 11.911° NNE |
| 12 mins | 2026-10-30 18:24:26.672Z | 178.883° S | 2026-10-30 18:29:26.672Z | 236.487° WSW | 61.711° | 2026-10-30 18:36:26.672Z | 338.2° N |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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