COSMOS 2246, 22647
Orbit data source: Space-Track
COSMOS 2246, 22647 is a payload satellite owned by VKS (CIS) in LEO that was launched on Tue, 11 May 1993 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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22647 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
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, 0.8 m
Radar Cross Section
1.257 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 COSMOS 2246
1 22647U 93030B 25346.77077746 .00000022 00000-0 61732-4 0 9998
2 22647 82.5860 75.9532 0009273 342.4939 17.5831 12.63630925502984Epoch: 2025-12-12T18:29Z
TLE epoch observation values (Epoch: 2025-12-12T18:29:55.172Z)
Latitude
-0.00012°
Longitude
76.76568°
Altitude
1,403.842 km
Speed
7.161 km/s
True Right ascension
05h 03m 48s
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
05:21:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.53 km
Perigee altitude
1,398.094 km
Semi-major axis
7,783.449 km
Eccentricity
0.00093
Inclination
82.586°
RAAN
75.9532°
Arg. of periapsis
342.4939°
True anomaly
17.61524°
Mean anomaly
17.5831°
Eccentric anomaly
17.59916°
Mean motion
3.16071 °/min
Orbital period
113.9 mins
BSTAR
0.000061732
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Other satellites on launch #30 in the year 1993 (1993-05-11 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 2246 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-12-13 07:54:31.962Z | 222.6° SW | 2025-12-13 08:01:31.962Z | 287.212° WNW | 31.851° | 2025-12-13 08:08:31.962Z | 351.239° N |
| 8 mins | 2025-12-13 16:02:31.962Z | 34.196° NE | 2025-12-13 16:06:31.962Z | 66.079° ENE | 16.019° | 2025-12-13 16:10:31.962Z | 96.421° ESE |
| 15 mins | 2025-12-13 17:55:31.962Z | 353.835° N | 2025-12-13 18:02:31.962Z | 132.029° SE | 44.837° | 2025-12-13 18:10:31.962Z | 172.758° S |
| 8 mins | 2025-12-13 19:52:31.962Z | 309.533° NW | 2025-12-13 19:55:31.962Z | 285.682° WNW | 16.782° | 2025-12-13 20:00:31.962Z | 246.872° WSW |
| 7 mins | 2025-12-14 04:52:31.962Z | 98.708° ESE | 2025-12-14 04:55:31.962Z | 75.16° E | 14.708° | 2025-12-14 04:59:31.962Z | 45.613° ENE |
| 11 mins | 2025-12-14 06:42:31.962Z | 182.809° SSW | 2025-12-14 06:48:31.962Z | 153.173° SSE | 44.774° | 2025-12-14 06:53:31.962Z | 9.12° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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