COSMOS 2272, 23003
Orbit data source: Space-Track
COSMOS 2272, 23003 is a payload satellite owned by VKS (CIS) in LEO that was launched on Sat, 12 Feb 1994 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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23003 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 COSMOS 2272
1 23003U 94011E 25257.55854861 .00000014 00000-0 19064-4 0 9995
2 23003 82.5678 108.0563 0012486 63.3420 296.8949 12.64391087457596
TLE epoch observation values (Epoch: 2025-09-14T13:24:18.599Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #11 in the year 1994 (1994-02-12 UTC)
COSMOS 2272 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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15 mins | 2025-09-15 14:11:01.728Z | 162.495° S | 2025-09-15 14:18:01.728Z | 94.001° ESE | 38.928° | 2025-09-15 14:26:01.728Z | 16.807° NNE |
12 mins | 2025-09-15 16:08:01.728Z | 238.7° WSW | 2025-09-15 16:13:01.728Z | 285.804° WNW | 27.129° | 2025-09-15 16:20:01.728Z | 347.55° N |
10 mins | 2025-09-16 00:13:01.728Z | 26.567° NE | 2025-09-16 00:18:01.728Z | 68.616° E | 19.601° | 2025-09-16 00:23:01.728Z | 108.337° ESE |
14 mins | 2025-09-16 02:07:01.728Z | 348.743° N | 2025-09-16 02:13:01.728Z | 297.01° NW | 44.234° | 2025-09-16 02:21:01.728Z | 181.165° SSW |
5 mins | 2025-09-16 04:05:01.728Z | 297.7° NW | 2025-09-16 04:07:01.728Z | 282.407° WNW | 12.888° | 2025-09-16 04:10:01.728Z | 260.441° W |
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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