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: 12 hours ago
TLE from 12 hours ago
0 COSMOS 1996
1 19787U 89009C 25258.86602448 .00000018 00000-0 41047-4 0 9997
2 19787 82.6181 180.6074 0006052 324.1322 96.0698 12.62916796686801Epoch: 2025-09-15T20:47Z
TLE epoch observation values (Epoch: 2025-09-15T20:47:04.515Z)
Latitude
59.53832°
Longitude
-113.56435°
Altitude
1,421.49 km
Speed
7.155 km/s
True Right ascension
12h 53m 04s
True Declination
59° 24' 02"
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
01:57:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.959 km
Perigee altitude
1,403.534 km
Semi-major axis
7,786.384 km
Eccentricity
0.00061
Inclination
82.6181°
RAAN
180.6074°
Arg. of periapsis
324.1322°
True anomaly
96.13876°
Mean anomaly
96.0698°
Eccentric anomaly
96.10428°
Mean motion
3.15893 °/min
Orbital period
113.96 mins
BSTAR
0.000041047
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-16 17:33:11.302Z | 97.417° ESE | 2025-09-16 17:36:11.302Z | 75.349° E | 12.748° | 2025-09-16 17:39:11.302Z | 53.321° ENE |
| 14 mins | 2025-09-16 19:23:11.302Z | 177.375° S | 2025-09-16 19:29:11.302Z | 126.3° SE | 44.102° | 2025-09-16 19:37:11.302Z | 10.745° NNE |
| 10 mins | 2025-09-16 21:21:11.302Z | 257.836° W | 2025-09-16 21:25:11.302Z | 291.563° WNW | 19.905° | 2025-09-16 21:31:11.302Z | 339.556° N |
| 12 mins | 2025-09-17 05:25:11.302Z | 19.762° NNE | 2025-09-17 05:30:11.302Z | 66.3° ENE | 27.211° | 2025-09-17 05:37:11.302Z | 127.998° SE |
| 14 mins | 2025-09-17 07:19:11.302Z | 340.554° N | 2025-09-17 07:26:11.302Z | 260.221° W | 39.006° | 2025-09-17 07:33:11.302Z | 196.955° 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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