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: 1 day ago
TLE from 1 day ago
0 NIMBUS 4
1 04362U 70025A 25287.51387311 -.00000003 00000-0 70369-4 0 9995
2 04362 99.9520 206.0158 0006825 233.9650 300.3950 13.44738101723826Epoch: 2025-10-14T12:19Z
TLE epoch observation values (Epoch: 2025-10-14T12:19:58.636Z)
Latitude
5.543°
Longitude
178.69095°
Altitude
1,091.326 km
Speed
7.308 km/s
True Right ascension
01h 47m 56s
True Declination
5° 30' 41"
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
13:20:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,094.099 km
Perigee altitude
1,083.906 km
Semi-major axis
7,467.14 km
Eccentricity
0.00068
Inclination
99.952°
RAAN
206.0158°
Arg. of periapsis
233.965°
True anomaly
300.32751°
Mean anomaly
300.395°
Eccentric anomaly
300.36126°
Mean motion
3.36366 °/min
Orbital period
107.03 mins
BSTAR
0.000070369
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-10-15 19:43:11.926Z | 213.139° SW | 2025-10-15 19:48:11.926Z | 268.977° W | 24.642° | 2025-10-15 19:53:11.926Z | 319.911° NNW |
| 11 mins | 2025-10-16 06:56:11.926Z | 32.606° NE | 2025-10-16 07:01:11.926Z | 93.521° ESE | 34.421° | 2025-10-16 07:07:11.926Z | 168.092° S |
| 10 mins | 2025-10-16 08:42:11.926Z | 350.665° N | 2025-10-16 08:47:11.926Z | 288.64° WNW | 28.426° | 2025-10-16 08:52:11.926Z | 237.08° WSW |
| 9 mins | 2025-10-16 17:12:11.926Z | 103.122° ESE | 2025-10-16 17:16:11.926Z | 59.37° ENE | 22.3° | 2025-10-16 17:21:11.926Z | 10.071° NNE |
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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