COSMOS 1994, 19785
Orbit data source: Space-Track
COSMOS 1994, 19785 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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19785 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: 11 hours ago
TLE from 11 hours ago
0 COSMOS 1994
1 19785U 89009A 26046.17547553 .00000040 00000-0 16139-3 0 9998
2 19785 82.6162 69.4901 0012064 223.5132 207.1988 12.64339622707969Epoch: 2026-02-15T04:12Z
TLE epoch observation values (Epoch: 2026-02-15T04:12:41.085Z)
Latitude
69.41018°
Longitude
-118.79385°
Altitude
1,425.426 km
Speed
7.151 km/s
True Right ascension
05h 58m 15s
True Declination
69° 18' 23"
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
18:23:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.786 km
Perigee altitude
1,393.014 km
Semi-major axis
7,780.537 km
Eccentricity
0.00121
Inclination
82.6162°
RAAN
69.4901°
Arg. of periapsis
223.5132°
True anomaly
207.1357°
Mean anomaly
207.1988°
Eccentric anomaly
207.16724°
Mean motion
3.16249 °/min
Orbital period
113.83 mins
BSTAR
0.00016139
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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 1994 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-02-16 00:50:13.769Z | 136.18° SSE | 2026-02-16 00:56:13.769Z | 86.908° E | 25.655° | 2026-02-16 01:03:13.769Z | 28.803° NE |
| 14 mins | 2026-02-16 02:44:13.769Z | 207.633° SW | 2026-02-16 02:51:13.769Z | 293.662° NW | 39.903° | 2026-02-16 02:58:13.769Z | 358.436° N |
| 14 mins | 2026-02-16 12:45:13.769Z | 4.326° NNE | 2026-02-16 12:51:13.769Z | 73.175° E | 40.455° | 2026-02-16 12:59:13.769Z | 156.366° SSE |
| 12 mins | 2026-02-16 14:40:13.769Z | 324.854° NNW | 2026-02-16 14:45:13.769Z | 281.68° WNW | 24.942° | 2026-02-16 14:52:13.769Z | 223.299° 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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