COSMOS 382, 4786
Orbit data source: Space-Track
COSMOS 382, 4786 is a payload satellite owned by TsKBEM (CIS) in LEO that was launched on Wed, 02 Dec 1970 UTC via a PROTON-K/D launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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4786 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
TsKBEM
Mission
Spacecraft
Bus & Motor
7K-L1E, Unknown motor
Mass
~19,040 kg wet, ~2,800 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: 10 hours ago
TLE from 10 hours ago
0 COSMOS 382
1 04786U 70103A 25346.87925721 -.00000022 00000-0 00000-0 0 9992
2 04786 55.8613 145.6553 1360151 234.1392 295.3372 8.42042053692876Epoch: 2025-12-12T21:06Z
TLE epoch observation values (Epoch: 2025-12-12T21:06:07.822Z)
Latitude
20.93521°
Longitude
-87.66382°
Altitude
3,401.1 km
Speed
6.519 km/s
True Right ascension
20h 42m 43s
True Declination
20° 51' 06"
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
05:22:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,215.645 km
Perigee altitude
2,439.398 km
Semi-major axis
10,205.659 km
Eccentricity
0.13602
Inclination
55.8613°
RAAN
145.6553°
Arg. of periapsis
234.1392°
True anomaly
280.32389°
Mean anomaly
295.3372°
Eccentric anomaly
287.92227°
Mean motion
2.10514 °/min
Orbital period
171.01 mins
BSTAR
0
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Other satellites on launch #103 in the year 1970 (1970-12-02 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.COSMOS 382 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. |
|---|---|---|---|---|---|---|---|
| 42 mins | 2025-12-13 09:54:08.970Z | 151.434° SSE | 2025-12-13 10:14:08.970Z | 101.318° ESE | 26.41° | 2025-12-13 10:36:08.970Z | 52.788° ENE |
| 56 mins | 2025-12-13 12:47:08.970Z | 214.305° SW | 2025-12-13 13:14:08.970Z | 123.599° SE | 44.921° | 2025-12-13 13:43:08.970Z | 47.464° ENE |
| 54 mins | 2025-12-13 15:55:08.970Z | 269.109° W | 2025-12-13 16:24:08.970Z | 347.224° N | 39.989° | 2025-12-13 16:49:08.970Z | 67.173° ENE |
| 48 mins | 2025-12-13 19:08:08.970Z | 306.003° NW | 2025-12-13 19:36:08.970Z | 27.541° NE | 43.108° | 2025-12-13 19:56:08.970Z | 115.846° SE |
| 37 mins | 2025-12-13 22:17:08.970Z | 311.66° NW | 2025-12-13 22:38:08.970Z | 249.154° W | 37.134° | 2025-12-13 22:54:08.970Z | 178.181° S |
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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