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: 13 hours ago
TLE from 13 hours ago
0 COSMOS 1994
1 19785U 89009A 25340.91741005 .00000018 00000-0 37192-4 0 9992
2 19785 82.6197 114.2408 0013086 31.3696 91.3289 12.64337759699082Epoch: 2025-12-06T22:01Z
TLE epoch observation values (Epoch: 2025-12-06T22:01:04.228Z)
Latitude
56.51471°
Longitude
-123.2003°
Altitude
1,414.73 km
Speed
7.158 km/s
True Right ascension
18h 52m 01s
True Declination
56° 22' 11"
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
09:11:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.589 km
Perigee altitude
1,392.226 km
Semi-major axis
7,780.545 km
Eccentricity
0.00131
Inclination
82.6197°
RAAN
114.2408°
Arg. of periapsis
31.3696°
True anomaly
91.47881°
Mean anomaly
91.3289°
Eccentric anomaly
91.40385°
Mean motion
3.16248 °/min
Orbital period
113.83 mins
BSTAR
0.000037192
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-07 18:53:21.708Z | 30.055° NE | 2025-12-07 18:57:21.708Z | 60.061° ENE | 14.78° | 2025-12-07 19:01:21.708Z | 90.641° ESE |
| 14 mins | 2025-12-07 20:47:21.708Z | 355.854° N | 2025-12-07 20:53:21.708Z | 47.01° ENE | 44.438° | 2025-12-07 21:01:21.708Z | 169.615° S |
| 9 mins | 2025-12-07 22:43:21.708Z | 314.453° NW | 2025-12-07 22:47:21.708Z | 282.173° WNW | 18.155° | 2025-12-07 22:52:21.708Z | 242.922° WSW |
| 5 mins | 2025-12-08 07:44:21.708Z | 93.173° ESE | 2025-12-08 07:46:21.708Z | 77.874° E | 13.273° | 2025-12-08 07:49:21.708Z | 55.091° ENE |
| 14 mins | 2025-12-08 09:33:21.708Z | 179.422° S | 2025-12-08 09:40:21.708Z | 60.368° ENE | 44.443° | 2025-12-08 09:47:21.708Z | 10.047° NNE |
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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