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, 0.9 m
Radar Cross Section
1.257 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 COSMOS 1994
1 19785U 89009A 26306.19046556 .00000040 00000-0 16111-3 0 9996
2 19785 82.6184 263.8865 0013079 1.1155 10.7812 12.64345557740824Epoch: 2026-11-02T04:34Z
TLE epoch observation values (Epoch: 2026-11-02T04:34:16.224Z)
Latitude
11.78331°
Longitude
155.38881°
Altitude
1,397.041 km
Speed
7.167 km/s
True Right ascension
17h 41m 42s
True Declination
11° 43' 13"
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
07:41:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.552 km
Perigee altitude
1,392.199 km
Semi-major axis
7,780.513 km
Eccentricity
0.00131
Inclination
82.6184°
RAAN
263.8865°
Arg. of periapsis
1.1155°
True anomaly
10.80928°
Mean anomaly
10.7812°
Eccentric anomaly
10.79524°
Mean motion
3.1625 °/min
Orbital period
113.83 mins
BSTAR
0.00016111
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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 | 2026-11-02 21:42:28.583Z | 170.387° S | 2026-11-02 21:48:28.583Z | 100.633° ESE | 67.836° | 2026-11-02 21:56:28.583Z | 13.046° NNE |
| 11 mins | 2026-11-02 23:39:28.583Z | 250.675° W | 2026-11-02 23:44:28.583Z | 295.908° NW | 24.483° | 2026-11-02 23:50:28.583Z | 343.655° N |
| 11 mins | 2026-11-03 07:43:28.583Z | 22.017° NNE | 2026-11-03 07:48:28.583Z | 66.128° ENE | 26.626° | 2026-11-03 07:54:28.583Z | 118.271° SE |
| 14 mins | 2026-11-03 09:37:28.583Z | 343.776° N | 2026-11-03 09:44:28.583Z | 254.2° W | 62.883° | 2026-11-03 09:51:28.583Z | 190.746° SSW |
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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