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: 8 hours ago
TLE from 8 hours ago
0 COSMOS 1913
1 18792U 88002E 25351.91289050 .00000023 00000-0 63062-4 0 9991
2 18792 82.5998 332.7226 0014580 118.3358 303.1415 12.65742279751827Epoch: 2025-12-17T21:54Z
TLE epoch observation values (Epoch: 2025-12-17T21:54:33.739Z)
Latitude
60.56379°
Longitude
-69.45437°
Altitude
1,403.426 km
Speed
7.167 km/s
True Right ascension
23h 03m 50s
True Declination
60° 25' 43"
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
04:50:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,407.983 km
Perigee altitude
1,385.312 km
Semi-major axis
7,774.785 km
Eccentricity
0.00146
Inclination
82.5998°
RAAN
332.7226°
Arg. of periapsis
118.3358°
True anomaly
303.00147°
Mean anomaly
303.1415°
Eccentric anomaly
303.0715°
Mean motion
3.166 °/min
Orbital period
113.71 mins
BSTAR
0.000063062
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-12-18 09:34:27.733Z | 11.814° NNE | 2025-12-18 09:41:27.733Z | 74.344° E | 27.953° | 2025-12-18 09:47:27.733Z | 127.988° SE |
| 14 mins | 2025-12-18 11:29:27.733Z | 339.968° N | 2025-12-18 11:36:27.733Z | 263.351° W | 38.002° | 2025-12-18 11:43:27.733Z | 198.791° SSW |
| 12 mins | 2025-12-18 22:22:27.733Z | 133.299° SE | 2025-12-18 22:27:27.733Z | 86.203° E | 27.217° | 2025-12-18 22:34:27.733Z | 27.203° NE |
| 14 mins | 2025-12-19 00:15:27.733Z | 211.485° SW | 2025-12-19 00:21:27.733Z | 273.151° WNW | 38.388° | 2025-12-19 00:29:27.733Z | 357.712° 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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