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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 COSMOS 2339
1 24727U 97006C 26308.06048175 .00000014 00000-0 19587-4 0 9993
2 24727 82.6050 166.4115 0001436 67.5414 85.5817 12.62381491369223Epoch: 2026-11-04T01:27Z
TLE epoch observation values (Epoch: 2026-11-04T01:27:05.623Z)
Latitude
26.65282°
Longitude
-82.39274°
Altitude
1,416.149 km
Speed
7.155 km/s
True Right ascension
22h 50m 46s
True Declination
26° 31' 37"
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
09:49:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.568 km
Perigee altitude
1,409.331 km
Semi-major axis
7,788.587 km
Eccentricity
0.00014
Inclination
82.605°
RAAN
166.4115°
Arg. of periapsis
67.5414°
True anomaly
85.59811°
Mean anomaly
85.5817°
Eccentric anomaly
85.5899°
Mean motion
3.15759 °/min
Orbital period
114.01 mins
BSTAR
0.000019587
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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 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-11-04 14:04:05.952Z | 133.674° SE | 2026-11-04 14:10:05.952Z | 84.348° E | 27.222° | 2026-11-04 14:16:05.952Z | 33.203° NE |
| 14 mins | 2026-11-04 15:58:05.952Z | 205.584° SW | 2026-11-04 16:05:05.952Z | 295.96° NW | 59.354° | 2026-11-04 16:12:05.952Z | 359.4° N |
| 15 mins | 2026-11-05 01:59:05.952Z | 2.679° NNE | 2026-11-05 02:06:05.952Z | 76.283° E | 56.694° | 2026-11-05 02:14:05.952Z | 155.116° SSE |
| 12 mins | 2026-11-05 03:55:05.952Z | 325.783° NNW | 2026-11-05 04:01:05.952Z | 270.893° WNW | 28.908° | 2026-11-05 04:07:05.952Z | 222.719° SW |
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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