COSMOS 2095, 20740
Orbit data source: Space-Track
COSMOS 2095, 20740 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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20740 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: 20 hours ago
TLE from 20 hours ago
0 COSMOS 2095
1 20740U 90070F 25257.98307667 .00000035 00000-0 13127-3 0 9991
2 20740 82.5679 84.5040 0018561 284.9455 188.8655 12.66132098622202Epoch: 2025-09-14T23:35Z
TLE epoch observation values (Epoch: 2025-09-14T23:35:37.824Z)
Latitude
65.23226°
Longitude
-99.93787°
Altitude
1,423.231 km
Speed
7.149 km/s
True Right ascension
16h 32m 39s
True Declination
65° 06' 45"
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
12:33:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,409.48 km
Perigee altitude
1,380.624 km
Semi-major axis
7,773.189 km
Eccentricity
0.00186
Inclination
82.5679°
RAAN
84.504°
Arg. of periapsis
284.9455°
True anomaly
188.8328°
Mean anomaly
188.8655°
Eccentric anomaly
188.84914°
Mean motion
3.16697 °/min
Orbital period
113.67 mins
BSTAR
0.00013127
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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 2095 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-15 22:22:53.304Z | 30.134° NE | 2025-09-15 22:26:53.304Z | 60.495° ENE | 15.341° | 2025-09-15 22:30:53.304Z | 91.449° ESE |
| 15 mins | 2025-09-16 00:15:53.304Z | 354.491° N | 2025-09-16 00:22:53.304Z | 60.833° ENE | 44.737° | 2025-09-16 00:30:53.304Z | 170.839° S |
| 8 mins | 2025-09-16 02:12:53.304Z | 311.546° NW | 2025-09-16 02:16:53.304Z | 278.769° WNW | 17.635° | 2025-09-16 02:20:53.304Z | 247.242° WSW |
| 5 mins | 2025-09-16 11:12:53.304Z | 91.153° ESE | 2025-09-16 11:14:53.304Z | 75.672° E | 13.565° | 2025-09-16 11:17:53.304Z | 53.167° ENE |
| 15 mins | 2025-09-16 13:00:53.304Z | 180.047° SSW | 2025-09-16 13:07:53.304Z | 115.092° SE | 44.613° | 2025-09-16 13:15:53.304Z | 9.853° NNE |
| 9 mins | 2025-09-16 14:59:53.304Z | 262.426° W | 2025-09-16 15:03:53.304Z | 296.697° NW | 19.095° | 2025-09-16 15:08:53.304Z | 336.429° NNW |
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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