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: 1 day ago
TLE from 1 day ago
0 COSMOS 1995
1 19786U 89009B 25306.43079440 .00000040 00000-0 16477-3 0 9996
2 19786 82.6241 172.5699 0002568 285.2236 248.9678 12.62226447691730Epoch: 2025-11-02T10:20Z
TLE epoch observation values (Epoch: 2025-11-02T10:20:20.636Z)
Latitude
5.71201°
Longitude
154.79905°
Altitude
1,416.66 km
Speed
7.152 km/s
True Right ascension
23h 27m 19s
True Declination
5° 40' 51"
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
06:51:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.088 km
Perigee altitude
1,409.087 km
Semi-major axis
7,789.224 km
Eccentricity
0.00026
Inclination
82.6241°
RAAN
172.5699°
Arg. of periapsis
285.2236°
True anomaly
248.94034°
Mean anomaly
248.9678°
Eccentric anomaly
248.95407°
Mean motion
3.1572 °/min
Orbital period
114.03 mins
BSTAR
0.00016477
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-03 14:05:57.675Z | 112.144° ESE | 2025-11-03 14:09:57.675Z | 81.444° E | 16.915° | 2025-11-03 14:14:57.675Z | 42.757° NE |
| 15 mins | 2025-11-03 15:56:57.675Z | 187.894° SSW | 2025-11-03 16:03:57.675Z | 237.877° WSW | 44.847° | 2025-11-03 16:11:57.675Z | 6.483° NNE |
| 8 mins | 2025-11-03 17:56:57.675Z | 269.868° W | 2025-11-03 18:00:57.675Z | 301.719° NW | 15.837° | 2025-11-03 18:04:57.675Z | 331.807° NNW |
| 14 mins | 2025-11-04 01:58:57.675Z | 10.151° NNE | 2025-11-04 02:05:57.675Z | 78.772° E | 32.175° | 2025-11-04 02:12:57.675Z | 139.237° SSE |
| 14 mins | 2025-11-04 03:53:57.675Z | 336.359° NNW | 2025-11-04 04:00:57.675Z | 266.457° W | 34.153° | 2025-11-04 04:07:57.675Z | 206.093° 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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