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: 7 hours ago
TLE from 7 hours ago
0 NIMBUS 4
1 04362U 70025A 26126.22051957 -.00000003 00000-0 71000-4 0 9993
2 04362 99.9619 47.7223 0008205 98.4741 61.0321 13.44753461751209Epoch: 2026-05-06T05:17Z
TLE epoch observation values (Epoch: 2026-05-06T05:17:32.890Z)
Latitude
20.09513°
Longitude
-72.08351°
Altitude
1,091.035 km
Speed
7.31 km/s
True Right ascension
15h 25m 33s
True Declination
19° 59' 22"
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
20:13:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,095.073 km
Perigee altitude
1,082.82 km
Semi-major axis
7,467.083 km
Eccentricity
0.00082
Inclination
99.9619°
RAAN
47.7223°
Arg. of periapsis
98.4741°
True anomaly
61.1144°
Mean anomaly
61.0321°
Eccentric anomaly
61.07325°
Mean motion
3.3637 °/min
Orbital period
107.03 mins
BSTAR
0.000071
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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 | 2026-05-06 17:10:07.750Z | 100.912° ESE | 2026-05-06 17:14:07.750Z | 59.252° ENE | 20.484° | 2026-05-06 17:18:07.750Z | 17.579° NNE |
| 11 mins | 2026-05-06 18:54:07.750Z | 176.894° S | 2026-05-06 18:59:07.750Z | 262.072° W | 42.823° | 2026-05-06 19:05:07.750Z | 338.971° N |
| 6 mins | 2026-05-07 06:10:07.750Z | 68.851° E | 2026-05-07 06:12:07.750Z | 89.468° E | 16.009° | 2026-05-07 06:16:07.750Z | 127.779° SE |
| 11 mins | 2026-05-07 07:53:07.750Z | 11.245° NNE | 2026-05-07 07:58:07.750Z | 316.619° NNW | 44.148° | 2026-05-07 08:04:07.750Z | 203.566° SW |
| 4 mins | 2026-05-07 09:41:07.750Z | 322.696° NNW | 2026-05-07 09:43:07.750Z | 303.313° NW | 13.427° | 2026-05-07 09:45:07.750Z | 284.444° WNW |
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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