COSMOS 2339, 24727
Orbit data source: Space-Track
COSMOS 2339, 24727 is a payload satellite owned by VKS (CIS) in LEO that was launched on Fri, 14 Feb 1997 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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24727 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 COSMOS 2339
1 24727U 97006C 25259.97431106 .00000006 00000-0 -25866-4 0 9996
2 24727 82.6000 69.0929 0000323 85.7929 28.8866 12.62372306317105
TLE epoch observation values (Epoch: 2025-09-16T23:23:00.475Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #6 in the year 1997 (1997-02-14 UTC)
COSMOS 2339 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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14 mins | 2025-09-17 22:12:58.268Z | 9.647° NNE | 2025-09-17 22:19:58.268Z | 77.404° E | 32.312° | 2025-09-17 22:26:58.268Z | 139.107° SSE |
13 mins | 2025-09-18 00:08:58.268Z | 332.694° NNW | 2025-09-18 00:14:58.268Z | 267.799° W | 34.047° | 2025-09-18 00:21:58.268Z | 206.478° SW |
13 mins | 2025-09-18 11:01:58.268Z | 144.934° SSE | 2025-09-18 11:07:58.268Z | 83.526° E | 32.295° | 2025-09-18 11:14:58.268Z | 23.193° NE |
14 mins | 2025-09-18 12:55:58.268Z | 219.93° SW | 2025-09-18 13:02:58.268Z | 291.299° WNW | 33.982° | 2025-09-18 13:09:58.268Z | 353.591° N |
6 mins | 2025-09-18 21:04:58.268Z | 40.45° NE | 2025-09-18 21:07:58.268Z | 63.953° ENE | 14.458° | 2025-09-18 21:10:58.268Z | 86.777° E |
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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