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: 22 hours ago
TLE from 22 hours ago
0 COSMOS 382
1 04786U 70103A 25305.62322241 -.00000023 00000-0 00000-0 0 9999
2 04786 55.8635 191.8644 1358908 210.4973 153.8287 8.42041861689407Epoch: 2025-11-01T14:57Z
TLE epoch observation values (Epoch: 2025-11-01T14:57:26.416Z)
Latitude
8.46304°
Longitude
-67.87629°
Altitude
5,103.244 km
Speed
5.513 km/s
True Right ascension
13h 10m 32s
True Declination
8° 25' 55"
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
08:56:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,214.378 km
Perigee altitude
2,440.668 km
Semi-major axis
10,205.66 km
Eccentricity
0.13589
Inclination
55.8635°
RAAN
191.8644°
Arg. of periapsis
210.4973°
True anomaly
159.77406°
Mean anomaly
153.8287°
Eccentric anomaly
156.88527°
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. |
|---|---|---|---|---|---|---|---|
| 51 mins | 2025-11-02 16:26:29.803Z | 175.01° S | 2025-11-02 16:52:29.803Z | 111.114° ESE | 35.747° | 2025-11-02 17:17:29.803Z | 48.716° ENE |
| 55 mins | 2025-11-02 19:26:29.803Z | 231.501° WSW | 2025-11-02 19:55:29.803Z | 315.016° NNW | 44.336° | 2025-11-02 20:21:29.803Z | 50.073° ENE |
| 47 mins | 2025-11-02 22:39:29.803Z | 283.962° WNW | 2025-11-02 23:06:29.803Z | 358.919° N | 38.688° | 2025-11-02 23:26:29.803Z | 77.362° E |
| 39 mins | 2025-11-03 01:51:29.803Z | 311.625° NW | 2025-11-03 02:14:29.803Z | 37.935° NE | 44.809° | 2025-11-03 02:30:29.803Z | 132.173° SE |
| 26 mins | 2025-11-03 04:58:29.803Z | 304.528° NW | 2025-11-03 05:12:29.803Z | 256.499° W | 25.7° | 2025-11-03 05:24:29.803Z | 201.824° SSW |
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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