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
CONE + 2 PAN, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 NIMBUS 4
1 04362U 70025A 26256.27099247 -.00000023 00000-0 37543-4 0 9992
2 04362 99.9566 176.5127 0007855 138.2165 14.6336 13.44758838768680Epoch: 2026-09-13T06:30Z
TLE epoch observation values (Epoch: 2026-09-13T06:30:13.749Z)
Latitude
26.72272°
Longitude
-88.26842°
Altitude
1,089.056 km
Speed
7.313 km/s
True Right ascension
00h 06m 13s
True Declination
26° 35' 28"
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
09:29:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,094.792 km
Perigee altitude
1,083.061 km
Semi-major axis
7,467.063 km
Eccentricity
0.00079
Inclination
99.9566°
RAAN
176.5127°
Arg. of periapsis
138.2165°
True anomaly
14.65636°
Mean anomaly
14.6336°
Eccentric anomaly
14.64498°
Mean motion
3.36371 °/min
Orbital period
107.02 mins
BSTAR
0.000037543
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-09-13 18:20:48.045Z | 152.407° SSE | 2026-09-13 18:26:48.045Z | 88.309° E | 68.564° | 2026-09-13 18:32:48.045Z | 350.961° N |
| 7 mins | 2026-09-13 20:09:48.045Z | 233.372° WSW | 2026-09-13 20:12:48.045Z | 264.201° W | 19.323° | 2026-09-13 20:16:48.045Z | 305.291° NW |
| 11 mins | 2026-09-14 07:21:48.045Z | 27.302° NE | 2026-09-14 07:26:48.045Z | 115.263° SE | 59.813° | 2026-09-14 07:32:48.045Z | 181.539° SSW |
| 8 mins | 2026-09-14 09:07:48.045Z | 341.034° N | 2026-09-14 09:11:48.045Z | 295.491° NW | 24.422° | 2026-09-14 09:15:48.045Z | 253.677° 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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