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: 5 hours ago
TLE from 5 hours ago
0 NIMBUS 4
1 04362U 70025A 26036.27137457 -.00000008 00000-0 62875-4 0 9993
2 04362 99.9610 318.6436 0007129 324.3734 201.3371 13.44747647739112Epoch: 2026-02-05T06:30Z
TLE epoch observation values (Epoch: 2026-02-05T06:30:46.762Z)
Latitude
14.07064°
Longitude
-91.96729°
Altitude
1,098.651 km
Speed
7.302 km/s
True Right ascension
09h 24m 36s
True Declination
13° 59' 36"
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
13:03:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,094.291 km
Perigee altitude
1,083.645 km
Semi-major axis
7,467.105 km
Eccentricity
0.00071
Inclination
99.961°
RAAN
318.6436°
Arg. of periapsis
324.3734°
True anomaly
201.3074°
Mean anomaly
201.3371°
Eccentric anomaly
201.32225°
Mean motion
3.36368 °/min
Orbital period
107.03 mins
BSTAR
0.000062875
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-05 16:37:40.512Z | 69.123° E | 2026-02-05 16:39:40.512Z | 50.585° ENE | 12.126° | 2026-02-05 16:41:40.512Z | 32.484° NE |
| 11 mins | 2026-02-05 18:18:40.512Z | 151.253° SSE | 2026-02-05 18:23:40.512Z | 77.528° E | 43.275° | 2026-02-05 18:29:40.512Z | 350.37° N |
| 7 mins | 2026-02-05 20:06:40.512Z | 235.181° WSW | 2026-02-05 20:09:40.512Z | 266.347° W | 17.973° | 2026-02-05 20:13:40.512Z | 306.518° NW |
| 12 mins | 2026-02-06 07:17:40.512Z | 24.512° NE | 2026-02-06 07:23:40.512Z | 122.538° SE | 40.829° | 2026-02-06 07:29:40.512Z | 182.311° SSW |
| 8 mins | 2026-02-06 09:04:40.512Z | 339.443° N | 2026-02-06 09:08:40.512Z | 293.177° NW | 22.27° | 2026-02-06 09:12:40.512Z | 252.852° W |
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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