COSMOS 1996, 19787
Orbit data source: Space-Track
COSMOS 1996, 19787 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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19787 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: 1 day ago
TLE from 1 day ago
0 COSMOS 1996
1 19787U 89009C 25306.02317773 .00000047 00000-0 20233-3 0 9998
2 19787 82.6121 150.6433 0005975 199.9907 313.3226 12.62918673692750Epoch: 2025-11-02T00:33Z
TLE epoch observation values (Epoch: 2025-11-02T00:33:22.555Z)
Latitude
26.53016°
Longitude
-82.93868°
Altitude
1,410.817 km
Speed
7.159 km/s
True Right ascension
21h 47m 48s
True Declination
26° 24' 16"
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
06:46:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.892 km
Perigee altitude
1,403.587 km
Semi-major axis
7,786.376 km
Eccentricity
0.0006
Inclination
82.6121°
RAAN
150.6433°
Arg. of periapsis
199.9907°
True anomaly
313.27276°
Mean anomaly
313.3226°
Eccentric anomaly
313.29768°
Mean motion
3.15893 °/min
Orbital period
113.96 mins
BSTAR
0.00020233
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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 1996 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 | 2025-11-03 13:51:38.455Z | 165.783° S | 2025-11-03 13:58:38.455Z | 101.948° ESE | 40.262° | 2025-11-03 14:06:38.455Z | 16.052° NNE |
| 12 mins | 2025-11-03 15:48:38.455Z | 238.849° WSW | 2025-11-03 15:54:38.455Z | 293.127° NW | 25.821° | 2025-11-03 16:00:38.455Z | 344.346° N |
| 11 mins | 2025-11-03 23:54:38.455Z | 25.336° NE | 2025-11-03 23:59:38.455Z | 68.342° E | 21.197° | 2025-11-04 00:05:38.455Z | 115.535° SE |
| 14 mins | 2025-11-04 01:48:38.455Z | 346.987° N | 2025-11-04 01:55:38.455Z | 242.808° WSW | 43.484° | 2025-11-04 02:02:38.455Z | 184.712° 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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