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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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, 0.9 m
Radar Cross Section
1.257 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 COSMOS 1995
1 19786U 89009B 26316.95214506 .00000020 00000-0 52677-4 0 9990
2 19786 82.6199 294.4083 0003992 130.4177 256.7480 12.62239453739114Epoch: 2026-11-12T22:51Z
TLE epoch observation values (Epoch: 2026-11-12T22:51:05.333Z)
Latitude
26.91282°
Longitude
-96.69103°
Altitude
1,417.572 km
Speed
7.154 km/s
True Right ascension
19h 52m 38s
True Declination
26° 47' 10"
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
09:53:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.143 km
Perigee altitude
1,407.924 km
Semi-major axis
7,789.171 km
Eccentricity
0.0004
Inclination
82.6199°
RAAN
294.4083°
Arg. of periapsis
130.4177°
True anomaly
256.70348°
Mean anomaly
256.748°
Eccentric anomaly
256.72574°
Mean motion
3.15723 °/min
Orbital period
114.02 mins
BSTAR
0.000052677
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-11-13 21:39:58.901Z | 119.776° SE | 2026-11-13 21:44:58.901Z | 81.118° E | 19.983° | 2026-11-13 21:49:58.901Z | 41.213° NE |
| 15 mins | 2026-11-13 23:31:58.901Z | 192.155° SSW | 2026-11-13 23:38:58.901Z | 263.96° W | 78.039° | 2026-11-13 23:46:58.901Z | 4.762° NNE |
| 7 mins | 2026-11-14 01:32:58.901Z | 278.597° WNW | 2026-11-14 01:35:58.901Z | 301.951° NW | 14.766° | 2026-11-14 01:39:58.901Z | 331.134° NNW |
| 14 mins | 2026-11-14 09:33:58.901Z | 8.623° NNE | 2026-11-14 09:40:58.901Z | 80.084° E | 42.871° | 2026-11-14 09:47:58.901Z | 142.767° SSE |
| 13 mins | 2026-11-14 11:29:58.901Z | 330.177° NNW | 2026-11-14 11:35:58.901Z | 266.476° W | 38.571° | 2026-11-14 11:42:58.901Z | 209.268° 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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