COSMOS 2385, 27056
Orbit data source: Space-Track
COSMOS 2385, 27056 is a payload satellite owned by KVR (CIS) in LEO that was launched on Fri, 28 Dec 2001 UTC via a TSIKLON-3 launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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27056 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 COSMOS 2385
1 27056U 01058B 25296.21559824 .00000044 00000-0 19139-3 0 9998
2 27056 82.5427 11.4124 0006891 57.3695 356.2518 12.60558874 95923
TLE epoch observation values (Epoch: 2025-10-23T05:10:27.687Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #58 in the year 2001 (2001-12-28 UTC)
COSMOS 2385 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. |
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16 mins | 2025-10-23 16:55:21.628Z | 353.836° N | 2025-10-23 17:03:21.628Z | 69.377° E | 44.769° | 2025-10-23 17:11:21.628Z | 170.887° S |
9 mins | 2025-10-23 18:53:21.628Z | 314.291° NW | 2025-10-23 18:57:21.628Z | 282.652° WNW | 17.636° | 2025-10-23 19:02:21.628Z | 244.004° WSW |
6 mins | 2025-10-24 03:55:21.628Z | 98.527° ESE | 2025-10-24 03:58:21.628Z | 75.339° E | 14.44° | 2025-10-24 04:01:21.628Z | 52.532° ENE |
15 mins | 2025-10-24 05:45:21.628Z | 182.042° SSW | 2025-10-24 05:52:21.628Z | 46.377° ENE | 44.724° | 2025-10-24 06:00:21.628Z | 8.975° NNE |
9 mins | 2025-10-24 07:44:21.628Z | 263.681° W | 2025-10-24 07:48:21.628Z | 296.872° NW | 18.214° | 2025-10-24 07:53:21.628Z | 335.905° NNW |
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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