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: 7 hours ago
TLE from 7 hours ago
0 COSMOS 1994
1 19785U 89009A 25291.14355817 .00000038 00000-0 14594-3 0 9996
2 19785 82.6200 145.9403 0013286 137.7965 346.9056 12.64335717692799Epoch: 2025-10-18T03:26Z
TLE epoch observation values (Epoch: 2025-10-18T03:26:43.425Z)
Latitude
54.74409°
Longitude
-123.12457°
Altitude
1,404.012 km
Speed
7.168 km/s
True Right ascension
21h 01m 44s
True Declination
54° 35' 43"
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
05:07:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.753 km
Perigee altitude
1,392.079 km
Semi-major axis
7,780.553 km
Eccentricity
0.00133
Inclination
82.62°
RAAN
145.9403°
Arg. of periapsis
137.7965°
True anomaly
346.87105°
Mean anomaly
346.9056°
Eccentric anomaly
346.88833°
Mean motion
3.16248 °/min
Orbital period
113.83 mins
BSTAR
0.00014594
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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 | 2025-10-18 14:16:17.022Z | 153.409° SSE | 2025-10-18 14:23:17.022Z | 93.859° ESE | 33.669° | 2025-10-18 14:30:17.022Z | 24.012° NE |
| 13 mins | 2025-10-18 16:12:17.022Z | 224.611° SW | 2025-10-18 16:18:17.022Z | 283.79° WNW | 32.572° | 2025-10-18 16:25:17.022Z | 350.936° N |
| 7 mins | 2025-10-19 00:19:17.022Z | 35.314° NE | 2025-10-19 00:22:17.022Z | 58.674° ENE | 15.06° | 2025-10-19 00:26:17.022Z | 90.057° ESE |
| 14 mins | 2025-10-19 02:12:17.022Z | 354.983° N | 2025-10-19 02:19:17.022Z | 130.824° SE | 44.493° | 2025-10-19 02:26:17.022Z | 170.726° S |
| 8 mins | 2025-10-19 04:09:17.022Z | 308.372° NW | 2025-10-19 04:12:17.022Z | 283.546° WNW | 17.396° | 2025-10-19 04:17:17.022Z | 244.335° 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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