COSMOS 1913, 18792
Orbit data source: Space-Track
COSMOS 1913, 18792 is a payload satellite owned by UNKS (CIS) in LEO that was launched on Fri, 15 Jan 1988 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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18792 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 COSMOS 1913
1 18792U 88002E 25356.02461914 .00000016 00000-0 28319-4 0 9997
2 18792 82.6002 330.0892 0014666 109.5141 318.3840 12.65742366752346Epoch: 2025-12-22T00:35Z
TLE epoch observation values (Epoch: 2025-12-22T00:35:27.093Z)
Latitude
66.72331°
Longitude
-112.12023°
Altitude
1,402.323 km
Speed
7.169 km/s
True Right ascension
23h 10m 17s
True Declination
66° 36' 31"
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
23:15:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,408.05 km
Perigee altitude
1,385.245 km
Semi-major axis
7,774.784 km
Eccentricity
0.00147
Inclination
82.6002°
RAAN
330.0892°
Arg. of periapsis
109.5141°
True anomaly
318.27223°
Mean anomaly
318.384°
Eccentric anomaly
318.32813°
Mean motion
3.166 °/min
Orbital period
113.71 mins
BSTAR
0.000028319
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Other satellites on launch #2 in the year 1988 (1988-01-15 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 1913 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-12-23 01:03:11.039Z | 255.268° W | 2025-12-23 01:08:11.039Z | 293.82° NW | 17.677° | 2025-12-23 01:13:11.039Z | 333.801° NNW |
| 13 mins | 2025-12-23 09:06:11.039Z | 14.704° NNE | 2025-12-23 09:12:11.039Z | 71.487° E | 29.01° | 2025-12-23 09:19:11.039Z | 132.952° SE |
| 13 mins | 2025-12-23 11:01:11.039Z | 336.485° NNW | 2025-12-23 11:07:11.039Z | 268.543° W | 37.102° | 2025-12-23 11:14:11.039Z | 201.157° SSW |
| 12 mins | 2025-12-23 21:53:11.039Z | 136.077° SSE | 2025-12-23 21:58:11.039Z | 89.226° E | 28.196° | 2025-12-23 22:05:11.039Z | 27.33° NE |
| 14 mins | 2025-12-23 23:46:11.039Z | 212.716° SW | 2025-12-23 23:53:11.039Z | 291.14° WNW | 37.469° | 2025-12-24 00:00:11.039Z | 356.324° N |
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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