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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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: 8 hours ago
TLE from 8 hours ago
0 NIMBUS 4
1 4362U 70025A 26085.71857361 -.00000021 00000-0 40932-4 0 9994
2 4362 99.9612 7.6105 0007195 193.5561 190.3557 13.44750839745767Epoch: 2026-03-26T17:14Z
TLE epoch observation values (Epoch: 2026-03-26T17:14:44.759Z)
Latitude
23.53674°
Longitude
-79.60437°
Altitude
1,099.643 km
Speed
7.302 km/s
True Right ascension
00h 12m 58s
True Declination
23° 25' 01"
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
06:03:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,094.329 km
Perigee altitude
1,083.583 km
Semi-major axis
7,467.093 km
Eccentricity
0.00072
Inclination
99.9612°
RAAN
7.6105°
Arg. of periapsis
193.5561°
True anomaly
190.34089°
Mean anomaly
190.3557°
Eccentric anomaly
190.34829°
Mean motion
3.36369 °/min
Orbital period
107.03 mins
BSTAR
0.000040932
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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 | 2026-03-27 06:16:08.764Z | 54.019° ENE | 2026-03-27 06:20:08.764Z | 95.35° ESE | 18.565° | 2026-03-27 06:24:08.764Z | 134.536° SE |
| 11 mins | 2026-03-27 08:01:08.764Z | 6.912° NNE | 2026-03-27 08:06:08.764Z | 275.229° WNW | 42.722° | 2026-03-27 08:12:08.764Z | 208.351° SW |
| 11 mins | 2026-03-27 18:15:08.764Z | 147.281° SSE | 2026-03-27 18:20:08.764Z | 63.955° ENE | 42.215° | 2026-03-27 18:26:08.764Z | 351.555° N |
| 7 mins | 2026-03-27 20:03:08.764Z | 235.78° WSW | 2026-03-27 20:06:08.764Z | 269.169° W | 19.571° | 2026-03-27 20:10:08.764Z | 309.482° NW |
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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