COSMOS 2338, 24726
Orbit data source: Space-Track
COSMOS 2338, 24726 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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24726 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 COSMOS 2338
1 24726U 97006B 25260.00681955 .00000038 00000-0 15365-3 0 9996
2 24726 82.5953 77.1549 0004964 359.3986 0.7098 12.61386697316030
TLE epoch observation values (Epoch: 2025-09-17T00:09:49.209Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #6 in the year 1997 (1997-02-14 UTC)
COSMOS 2338 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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10 mins | 2025-09-18 01:33:42.138Z | 319.236° NNW | 2025-09-18 01:38:42.138Z | 280.506° WNW | 18.102° | 2025-09-18 01:43:42.138Z | 242.14° WSW |
6 mins | 2025-09-18 10:36:42.138Z | 93.718° ESE | 2025-09-18 10:38:42.138Z | 78.288° E | 13.988° | 2025-09-18 10:42:42.138Z | 48.581° ENE |
15 mins | 2025-09-18 12:25:42.138Z | 180.936° SSW | 2025-09-18 12:32:42.138Z | 87.534° E | 44.779° | 2025-09-18 12:40:42.138Z | 9.347° NNE |
9 mins | 2025-09-18 14:24:42.138Z | 261.684° W | 2025-09-18 14:28:42.138Z | 294.896° NW | 18.671° | 2025-09-18 14:33:42.138Z | 334.863° NNW |
13 mins | 2025-09-18 22:28:42.138Z | 17.025° NNE | 2025-09-18 22:34:42.138Z | 76.364° E | 29.005° | 2025-09-18 22:41:42.138Z | 133.772° SE |
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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