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: 8 hours ago
TLE from 8 hours ago
0 COSMOS 1995
1 19786U 89009B 25260.90833926 .00000013 00000-0 12931-4 0 9996
2 19786 82.6256 201.4179 0004273 33.8612 29.0222 12.62224445685991Epoch: 2025-09-17T21:48Z
TLE epoch observation values (Epoch: 2025-09-17T21:48:00.512Z)
Latitude
62.08048°
Longitude
-108.59628°
Altitude
1,421.466 km
Speed
7.157 km/s
True Right ascension
14h 21m 56s
True Declination
61° 57' 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
22:18:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.424 km
Perigee altitude
1,407.767 km
Semi-major axis
7,789.232 km
Eccentricity
0.00043
Inclination
82.6256°
RAAN
201.4179°
Arg. of periapsis
33.8612°
True anomaly
29.04597°
Mean anomaly
29.0222°
Eccentric anomaly
29.03408°
Mean motion
3.15719 °/min
Orbital period
114.03 mins
BSTAR
0.000012931
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-09-18 07:36:12.535Z | 1.683° NNE | 2025-09-18 07:43:12.535Z | 93.112° ESE | 41.535° | 2025-09-18 07:50:12.535Z | 158.424° S |
| 11 mins | 2025-09-18 09:32:12.535Z | 321.179° NNW | 2025-09-18 09:37:12.535Z | 276.865° WNW | 23.563° | 2025-09-18 09:43:12.535Z | 228.179° WSW |
| 14 mins | 2025-09-18 20:24:12.535Z | 167.42° S | 2025-09-18 20:30:12.535Z | 100.07° ESE | 41.888° | 2025-09-18 20:38:12.535Z | 14.204° NNE |
| 11 mins | 2025-09-18 22:21:12.535Z | 247.723° W | 2025-09-18 22:26:12.535Z | 293.682° NW | 23.867° | 2025-09-18 22:32:12.535Z | 343.348° N |
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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