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: 1 day ago
TLE from 1 day ago
0 NIMBUS 4
1 04362U 70025A 26305.52800419 -.00000017 00000-0 46703-4 0 9997
2 04362 99.9612 225.2900 0007900 27.4287 145.2662 13.44761215775301Epoch: 2026-11-01T12:40Z
TLE epoch observation values (Epoch: 2026-11-01T12:40:19.562Z)
Latitude
7.07445°
Longitude
175.63294°
Altitude
1,098.579 km
Speed
7.301 km/s
True Right ascension
03h 06m 07s
True Declination
7° 02' 04"
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
08:55:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,094.817 km
Perigee altitude
1,083.019 km
Semi-major axis
7,467.055 km
Eccentricity
0.00079
Inclination
99.9612°
RAAN
225.29°
Arg. of periapsis
27.4287°
True anomaly
145.31774°
Mean anomaly
145.2662°
Eccentric anomaly
145.29197°
Mean motion
3.36371 °/min
Orbital period
107.02 mins
BSTAR
0.000046703
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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 | 2026-11-02 18:17:13.280Z | 147.649° SSE | 2026-11-02 18:22:13.280Z | 92.037° ESE | 61.734° | 2026-11-02 18:29:13.280Z | 351.425° N |
| 8 mins | 2026-11-02 20:05:13.280Z | 229.863° WSW | 2026-11-02 20:08:13.280Z | 261.735° W | 21.162° | 2026-11-02 20:13:13.280Z | 312.719° NW |
| 11 mins | 2026-11-03 07:17:13.280Z | 29.077° NE | 2026-11-03 07:22:13.280Z | 106.352° ESE | 55.173° | 2026-11-03 07:28:13.280Z | 177.799° S |
| 9 mins | 2026-11-03 09:03:13.280Z | 343.735° N | 2026-11-03 09:07:13.280Z | 297.926° NW | 26.834° | 2026-11-03 09:12:13.280Z | 246.391° 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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