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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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Non-operational Defense Communications
Bus & Motor
STRELA-3, Unknown motor
Mass
225 kg wet, 225 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 1 Ant, 3.5 m
Radar Cross Section
1.583 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 COSMOS 2338
1 24726U 97006B 25307.99378292 .00000018 00000-0 39736-4 0 9990
2 24726 82.6031 46.6704 0004392 230.3651 129.7052 12.61388201322081Epoch: 2025-11-03T23:51Z
TLE epoch observation values (Epoch: 2025-11-03T23:51:02.844Z)
Latitude
-0.00005°
Longitude
5.42136°
Altitude
1,422.137 km
Speed
7.149 km/s
True Right ascension
03h 06m 40s
True Declination
0° 00' 00"
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
06:56:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,417.963 km
Perigee altitude
1,411.118 km
Semi-major axis
7,792.678 km
Eccentricity
0.00044
Inclination
82.6031°
RAAN
46.6704°
Arg. of periapsis
230.3651°
True anomaly
129.74391°
Mean anomaly
129.7052°
Eccentric anomaly
129.72455°
Mean motion
3.1551 °/min
Orbital period
114.1 mins
BSTAR
0.000039736
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Other satellites on launch #6 in the year 1997 (1997-02-14 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 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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2025-11-04 17:35:03.543Z | 6.767° NNE | 2025-11-04 17:43:03.543Z | 81.273° E | 32.376° | 2025-11-04 17:50:03.543Z | 140.165° SSE |
| 14 mins | 2025-11-04 19:31:03.543Z | 335.806° NNW | 2025-11-04 19:38:03.543Z | 265.236° W | 33.823° | 2025-11-04 19:45:03.543Z | 206.315° SW |
| 13 mins | 2025-11-05 06:25:03.543Z | 146.914° SSE | 2025-11-05 06:31:03.543Z | 88.922° E | 32.724° | 2025-11-05 06:38:03.543Z | 24.094° NE |
| 13 mins | 2025-11-05 08:20:03.543Z | 222.895° SW | 2025-11-05 08:26:03.543Z | 283.87° WNW | 33.779° | 2025-11-05 08:33:03.543Z | 351.741° N |
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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