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: 12 hours ago
TLE from 12 hours ago
0 COSMOS 1994
1 19785U 89009A 25311.01566750 .00000011 00000-0 45335-6 0 9996
2 19785 82.6179 133.2848 0013721 95.5152 74.0539 12.64336635695305Epoch: 2025-11-07T00:22Z
TLE epoch observation values (Epoch: 2025-11-07T00:22:33.671Z)
Latitude
10.14316°
Longitude
-100.14279°
Altitude
1,404.17 km
Speed
7.16 km/s
True Right ascension
20h 47m 51s
True Declination
10° 05' 19"
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
08:07:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.088 km
Perigee altitude
1,391.737 km
Semi-major axis
7,780.549 km
Eccentricity
0.00137
Inclination
82.6179°
RAAN
133.2848°
Arg. of periapsis
95.5152°
True anomaly
74.20515°
Mean anomaly
74.0539°
Eccentric anomaly
74.12952°
Mean motion
3.16248 °/min
Orbital period
113.83 mins
BSTAR
4.5335e-7
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2025-11-07 12:51:38.374Z | 179.357° S | 2025-11-07 12:59:38.374Z | 64.157° ENE | 44.37° | 2025-11-07 13:06:38.374Z | 10.339° NNE |
| 10 mins | 2025-11-07 14:50:38.374Z | 257.777° W | 2025-11-07 14:54:38.374Z | 290.886° WNW | 19.27° | 2025-11-07 15:00:38.374Z | 338.951° N |
| 12 mins | 2025-11-07 22:53:38.374Z | 16.943° NNE | 2025-11-07 22:59:38.374Z | 73.418° E | 27.346° | 2025-11-07 23:05:38.374Z | 126.555° SE |
| 13 mins | 2025-11-08 00:48:38.374Z | 338.303° N | 2025-11-08 00:54:38.374Z | 267.747° W | 38.784° | 2025-11-08 01:01:38.374Z | 198.082° SSW |
| 11 mins | 2025-11-08 11:41:38.374Z | 132.24° SE | 2025-11-08 11:46:38.374Z | 85.249° E | 26.806° | 2025-11-08 11:52:38.374Z | 31.548° NE |
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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