COSMOS 2093, 20738
Orbit data source: Space-Track
COSMOS 2093, 20738 is a payload satellite owned by UNKS (CIS) in LEO that was launched on Wed, 08 Aug 1990 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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20738 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 COSMOS 2093
1 20738U 90070D 25322.38787674 .00000006 00000-0 -25203-4 0 9993
2 20738 82.5749 75.9220 0008386 221.2533 201.4193 12.64088208627740Epoch: 2025-11-18T09:18Z
TLE epoch observation values (Epoch: 2025-11-18T09:18:32.550Z)
Latitude
61.80915°
Longitude
-107.38697°
Altitude
1,422.738 km
Speed
7.152 km/s
True Right ascension
05h 59m 41s
True Declination
61° 40' 41"
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
06:33:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,409.96 km
Perigee altitude
1,396.908 km
Semi-major axis
7,781.571 km
Eccentricity
0.00084
Inclination
82.5749°
RAAN
75.922°
Arg. of periapsis
221.2533°
True anomaly
201.38424°
Mean anomaly
201.4193°
Eccentric anomaly
201.40177°
Mean motion
3.16186 °/min
Orbital period
113.86 mins
BSTAR
-0.000025203
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Other satellites on launch #70 in the year 1990 (1990-08-08 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 2093 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-11-19 09:47:19.175Z | 232.721° WSW | 2025-11-19 09:54:19.175Z | 290.715° WNW | 26.06° | 2025-11-19 10:00:19.175Z | 343.528° N |
| 10 mins | 2025-11-19 17:54:19.175Z | 26.971° NE | 2025-11-19 17:59:19.175Z | 70.611° E | 20.834° | 2025-11-19 18:04:19.175Z | 110.994° ESE |
| 15 mins | 2025-11-19 19:47:19.175Z | 347.941° N | 2025-11-19 19:54:19.175Z | 279.932° WNW | 43.812° | 2025-11-19 20:02:19.175Z | 183.724° SSW |
| 4 mins | 2025-11-19 21:46:19.175Z | 296.34° NW | 2025-11-19 21:47:19.175Z | 288.964° WNW | 11.729° | 2025-11-19 21:50:19.175Z | 267.013° W |
| 10 mins | 2025-11-20 06:42:19.175Z | 118.723° SE | 2025-11-20 06:47:19.175Z | 77.17° E | 19.966° | 2025-11-20 06:52:19.175Z | 38.028° NE |
| 14 mins | 2025-11-20 08:34:19.175Z | 195.414° SSW | 2025-11-20 08:41:19.175Z | 302.357° NW | 43.722° | 2025-11-20 08:48:19.175Z | 3.353° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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