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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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: 14 hours ago
TLE from 14 hours ago
0 COSMOS 1994
1 19785U 89009A 25356.82214454 .00000028 00000-0 92558-4 0 9990
2 19785 82.6210 104.1135 0012468 355.6543 123.0933 12.64338099701091Epoch: 2025-12-22T19:43Z
TLE epoch observation values (Epoch: 2025-12-22T19:43:53.288Z)
Latitude
60.37121°
Longitude
-116.56902°
Altitude
1,420.639 km
Speed
7.154 km/s
True Right ascension
18h 04m 04s
True Declination
60° 14' 09"
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
08:34:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.107 km
Perigee altitude
1,392.705 km
Semi-major axis
7,780.543 km
Eccentricity
0.00125
Inclination
82.621°
RAAN
104.1135°
Arg. of periapsis
355.6543°
True anomaly
123.21289°
Mean anomaly
123.0933°
Eccentric anomaly
123.15311°
Mean motion
3.16248 °/min
Orbital period
113.83 mins
BSTAR
0.000092558
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-12-23 18:31:09.544Z | 6.779° NNE | 2025-12-23 18:37:09.544Z | 69.913° E | 37.975° | 2025-12-23 18:45:09.544Z | 150.894° SSE |
| 12 mins | 2025-12-23 20:26:09.544Z | 328.12° NNW | 2025-12-23 20:32:09.544Z | 271.837° WNW | 28.004° | 2025-12-23 20:38:09.544Z | 220.182° SW |
| 14 mins | 2025-12-24 07:17:09.544Z | 159.199° S | 2025-12-24 07:24:09.544Z | 85.104° E | 37.775° | 2025-12-24 07:31:09.544Z | 19.092° NNE |
| 13 mins | 2025-12-24 09:13:09.544Z | 233.391° WSW | 2025-12-24 09:19:09.544Z | 290.572° WNW | 28.415° | 2025-12-24 09:26:09.544Z | 349.866° 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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