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, 0.8 m
Radar Cross Section
1.257 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 COSMOS 1995
1 19786U 89009B 26126.27400407 .00000038 00000-0 15044-3 0 9996
2 19786 82.6244 55.3396 0002446 200.1372 328.0496 12.62234234715050Epoch: 2026-05-06T06:34Z
TLE epoch observation values (Epoch: 2026-05-06T06:34:33.951Z)
Latitude
11.6871°
Longitude
-88.96548°
Altitude
1,414.099 km
Speed
7.155 km/s
True Right ascension
15h 35m 15s
True Declination
11° 37' 29"
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
20:14:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.96 km
Perigee altitude
1,409.15 km
Semi-major axis
7,789.192 km
Eccentricity
0.00024
Inclination
82.6244°
RAAN
55.3396°
Arg. of periapsis
200.1372°
True anomaly
328.03476°
Mean anomaly
328.0496°
Eccentric anomaly
328.04218°
Mean motion
3.15722 °/min
Orbital period
114.02 mins
BSTAR
0.00015044
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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 | 2026-05-06 19:06:07.490Z | 152.074° SSE | 2026-05-06 19:13:07.490Z | 83.675° E | 34.19° | 2026-05-06 19:20:07.490Z | 21.866° NNE |
| 13 mins | 2026-05-06 21:02:07.490Z | 227.199° WSW | 2026-05-06 21:08:07.490Z | 290.098° WNW | 32.236° | 2026-05-06 21:15:07.490Z | 352.053° N |
| 7 mins | 2026-05-07 05:10:07.490Z | 38.962° NE | 2026-05-07 05:13:07.490Z | 63.134° ENE | 15.858° | 2026-05-07 05:17:07.490Z | 94.026° ESE |
| 15 mins | 2026-05-07 07:02:07.490Z | 353.83° N | 2026-05-07 07:09:07.490Z | 46.144° ENE | 44.85° | 2026-05-07 07:17:07.490Z | 172.287° S |
| 8 mins | 2026-05-07 09:00:07.490Z | 306.804° NW | 2026-05-07 09:03:07.490Z | 282.221° WNW | 16.958° | 2026-05-07 09:08:07.490Z | 244.347° WSW |
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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