COSMOS 2248, 22649
Orbit data source: Space-Track
COSMOS 2248, 22649 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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22649 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: 13 hours ago
TLE from 13 hours ago
0 COSMOS 2248
1 22649U 93030D 26034.51935617 .00000018 00000-0 38712-4 0 9994
2 22649 82.5767 36.7937 0008212 231.8334 128.2019 12.63518842509537Epoch: 2026-02-03T12:27Z
TLE epoch observation values (Epoch: 2026-02-03T12:27:52.373Z)
Latitude
0.00005°
Longitude
76.12636°
Altitude
1,415.144 km
Speed
7.151 km/s
True Right ascension
02h 27m 10s
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
03:32:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.165 km
Perigee altitude
1,399.381 km
Semi-major axis
7,783.91 km
Eccentricity
0.00082
Inclination
82.5767°
RAAN
36.7937°
Arg. of periapsis
231.8334°
True anomaly
128.2758°
Mean anomaly
128.2019°
Eccentric anomaly
128.23886°
Mean motion
3.16043 °/min
Orbital period
113.91 mins
BSTAR
0.000038712
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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 2248 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 | 2026-02-04 01:52:51.719Z | 224.951° SW | 2026-02-04 01:59:51.719Z | 290.867° WNW | 31.106° | 2026-02-04 02:06:51.719Z | 351.536° N |
| 8 mins | 2026-02-04 10:00:51.719Z | 35.047° NE | 2026-02-04 10:03:51.719Z | 59.085° ENE | 16.618° | 2026-02-04 10:08:51.719Z | 98.336° ESE |
| 14 mins | 2026-02-04 11:53:51.719Z | 352.949° N | 2026-02-04 12:00:51.719Z | 165.32° S | 44.737° | 2026-02-04 12:07:51.719Z | 174.139° S |
| 7 mins | 2026-02-04 13:50:51.719Z | 307.954° NW | 2026-02-04 13:53:51.719Z | 284.191° WNW | 16.001° | 2026-02-04 13:57:51.719Z | 252.827° W |
| 7 mins | 2026-02-04 22:50:51.719Z | 98.157° ESE | 2026-02-04 22:53:51.719Z | 74.002° E | 15.526° | 2026-02-04 22:57:51.719Z | 44.418° NE |
| 15 mins | 2026-02-05 00:39:51.719Z | 184.673° SSW | 2026-02-05 00:46:51.719Z | 172.292° S | 44.931° | 2026-02-05 00:54:51.719Z | 7.91° 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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