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: 7 hours ago
TLE from 7 hours ago
0 COSMOS 1995
1 19786U 89009B 25363.80510044 .00000035 00000-0 13543-3 0 9995
2 19786 82.6233 136.1933 0004024 139.4377 334.7279 12.62229583698971Epoch: 2025-12-29T19:19Z
TLE epoch observation values (Epoch: 2025-12-29T19:19:20.678Z)
Latitude
64.89817°
Longitude
-88.10167°
Altitude
1,422.087 km
Speed
7.157 km/s
True Right ascension
20h 00m 55s
True Declination
64° 46' 37"
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
02:20:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.209 km
Perigee altitude
1,407.94 km
Semi-major axis
7,789.211 km
Eccentricity
0.0004
Inclination
82.6233°
RAAN
136.1933°
Arg. of periapsis
139.4377°
True anomaly
334.70821°
Mean anomaly
334.7279°
Eccentric anomaly
334.71805°
Mean motion
3.15721 °/min
Orbital period
114.02 mins
BSTAR
0.00013543
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-12-30 08:09:50.887Z | 122.725° SE | 2025-12-30 08:14:50.887Z | 82.903° E | 20.472° | 2025-12-30 08:20:50.887Z | 35.492° NE |
| 14 mins | 2025-12-30 10:02:50.887Z | 196.914° SSW | 2025-12-30 10:08:50.887Z | 259.68° W | 43.502° | 2025-12-30 10:16:50.887Z | 3.103° NNE |
| 5 mins | 2025-12-30 12:03:50.887Z | 285.308° WNW | 2025-12-30 12:05:50.887Z | 300.485° NW | 12.967° | 2025-12-30 12:08:50.887Z | 322.721° NNW |
| 14 mins | 2025-12-30 20:03:50.887Z | 6.553° NNE | 2025-12-30 20:10:50.887Z | 77.999° E | 36.027° | 2025-12-30 20:17:50.887Z | 145.431° SSE |
| 12 mins | 2025-12-30 21:59:50.887Z | 329.122° NNW | 2025-12-30 22:05:50.887Z | 269.032° W | 30.077° | 2025-12-30 22:11:50.887Z | 216.219° 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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