COSMOS 1995, 19786
Orbit data source: Space-Track
COSMOS 1995, 19786 is a payload satellite owned by UNKS (CIS) in LEO that was launched on Fri, 10 Feb 1989 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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19786 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: 12 hours ago
TLE from 12 hours ago
0 COSMOS 1995
1 19786U 89009B 25356.90926517 .00000027 00000-0 89376-4 0 9993
2 19786 82.6226 140.5651 0003866 152.0958 322.8548 12.62229302698109Epoch: 2025-12-22T21:49Z
TLE epoch observation values (Epoch: 2025-12-22T21:49:20.510Z)
Latitude
64.15664°
Longitude
-113.89727°
Altitude
1,422.377 km
Speed
7.157 km/s
True Right ascension
20h 20m 33s
True Declination
64° 01' 59"
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
08:34:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.087 km
Perigee altitude
1,408.064 km
Semi-major axis
7,789.213 km
Eccentricity
0.00039
Inclination
82.6226°
RAAN
140.5651°
Arg. of periapsis
152.0958°
True anomaly
322.82804°
Mean anomaly
322.8548°
Eccentric anomaly
322.84142°
Mean motion
3.15721 °/min
Orbital period
114.02 mins
BSTAR
0.000089376
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Other satellites on launch #9 in the year 1989 (1989-02-10 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 1995 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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2025-12-23 10:37:09.064Z | 189.549° SSW | 2025-12-23 10:45:09.064Z | 320.303° NNW | 44.514° | 2025-12-23 10:52:09.064Z | 5.458° NNE |
| 7 mins | 2025-12-23 12:38:09.064Z | 274.978° WNW | 2025-12-23 12:41:09.064Z | 298.652° NW | 15.176° | 2025-12-23 12:45:09.064Z | 329.056° NNW |
| 13 mins | 2025-12-23 20:40:09.064Z | 12.182° NNE | 2025-12-23 20:46:09.064Z | 73.484° E | 33.131° | 2025-12-23 20:53:09.064Z | 139.567° SSE |
| 13 mins | 2025-12-23 22:35:09.064Z | 333.021° NNW | 2025-12-23 22:41:09.064Z | 272.316° WNW | 33.249° | 2025-12-23 22:48:09.064Z | 208.637° 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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