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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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: 1 day ago
TLE from 1 day ago
0 COSMOS 1996
1 19787U 89009C 26262.07749101 .00000014 00000-0 15958-4 0 9992
2 19787 82.6132 306.5139 0006294 186.6002 199.3529 12.62927515733288Epoch: 2026-09-19T01:51Z
TLE epoch observation values (Epoch: 2026-09-19T01:51:35.223Z)
Latitude
25.72762°
Longitude
-75.81016°
Altitude
1,418.489 km
Speed
7.151 km/s
True Right ascension
20h 40m 18s
True Declination
25° 36' 17"
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
18:20:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.104 km
Perigee altitude
1,403.302 km
Semi-major axis
7,786.34 km
Eccentricity
0.00063
Inclination
82.6132°
RAAN
306.5139°
Arg. of periapsis
186.6002°
True anomaly
199.32902°
Mean anomaly
199.3529°
Eccentric anomaly
199.34096°
Mean motion
3.15895 °/min
Orbital period
113.96 mins
BSTAR
0.000015958
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2026-09-20 02:32:06.918Z | 142.452° SSE | 2026-09-20 02:39:06.918Z | 84.374° E | 32.004° | 2026-09-20 02:46:06.918Z | 26.473° NE |
| 14 mins | 2026-09-20 04:27:06.918Z | 212.138° SW | 2026-09-20 04:34:06.918Z | 293.859° NW | 51.441° | 2026-09-20 04:41:06.918Z | 356.873° N |
| 15 mins | 2026-09-20 14:28:06.918Z | 0.414° NNE | 2026-09-20 14:35:06.918Z | 86.955° E | 65.131° | 2026-09-20 14:43:06.918Z | 161.184° S |
| 11 mins | 2026-09-20 16:24:06.918Z | 321.424° NNW | 2026-09-20 16:29:06.918Z | 278.385° WNW | 24.798° | 2026-09-20 16:35:06.918Z | 229.819° 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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