NIMBUS 4, 4362
Orbit data source: Space-Track
NIMBUS 4, 4362 is a payload satellite owned by GSFC (US) in SSO that was launched on Wed, 08 Apr 1970 UTC via a THORAD SLV-2G AGENA D 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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4362 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
GE/MSVD
Mission
Non-operational spacecraft
Bus & Motor
NIMBUS, Unknown motor
Mass
619 kg wet, 619 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 NIMBUS 4
1 04362U 70025A 25310.69703389 .00000000 00000-0 76244-4 0 9992
2 04362 99.9546 228.9602 0007418 174.6172 214.3240 13.44740057726945Epoch: 2025-11-06T16:43Z
TLE epoch observation values (Epoch: 2025-11-06T16:43:43.728Z)
Latitude
28.46254°
Longitude
-73.55529°
Altitude
1,099.639 km
Speed
7.303 km/s
True Right ascension
14h 54m 06s
True Declination
28° 19' 31"
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
05:19:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,094.535 km
Perigee altitude
1,083.456 km
Semi-major axis
7,467.133 km
Eccentricity
0.00074
Inclination
99.9546°
RAAN
228.9602°
Arg. of periapsis
174.6172°
True anomaly
214.27611°
Mean anomaly
214.324°
Eccentric anomaly
214.30005°
Mean motion
3.36366 °/min
Orbital period
107.03 mins
BSTAR
0.000076244
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Other satellites on launch #25 in the year 1970 (1970-04-08 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 4 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-07 09:15:06.603Z | 338.614° N | 2025-11-07 09:19:06.603Z | 296.827° NW | 18.649° | 2025-11-07 09:23:06.603Z | 258.999° W |
| 11 mins | 2025-11-07 17:43:06.603Z | 127.867° SE | 2025-11-07 17:48:06.603Z | 66.485° ENE | 32.788° | 2025-11-07 17:54:06.603Z | 359.914° N |
| 10 mins | 2025-11-07 19:29:06.603Z | 205.597° SW | 2025-11-07 19:34:06.603Z | 271.098° WNW | 29.803° | 2025-11-07 19:39:06.603Z | 324.667° NNW |
| 9 mins | 2025-11-08 06:43:06.603Z | 44.568° NE | 2025-11-08 06:47:06.603Z | 96.056° ESE | 28.909° | 2025-11-08 06:52:06.603Z | 155.264° SSE |
| 10 mins | 2025-11-08 08:28:06.603Z | 354.943° N | 2025-11-08 08:33:06.603Z | 284.904° WNW | 33.393° | 2025-11-08 08:38:06.603Z | 228.871° WSW |
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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