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 25260.86491875 .00000028 00000-0 94722-4 0 9996
2 18792 82.6021 31.0129 0012923 332.0607 142.1515 12.65737352740306Epoch: 2025-09-17T20:45Z
TLE epoch observation values (Epoch: 2025-09-17T20:45:28.979Z)
Latitude
64.74295°
Longitude
-113.28633°
Altitude
1,418.433 km
Speed
7.154 km/s
True Right ascension
13h 00m 28s
True Declination
64° 37' 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
19:29:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,406.715 km
Perigee altitude
1,386.62 km
Semi-major axis
7,774.805 km
Eccentricity
0.00129
Inclination
82.6021°
RAAN
31.0129°
Arg. of periapsis
332.0607°
True anomaly
142.24225°
Mean anomaly
142.1515°
Eccentric anomaly
142.19688°
Mean motion
3.16599 °/min
Orbital period
113.71 mins
BSTAR
0.000094722
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-09-19 08:17:52.174Z | 145.279° SSE | 2025-09-19 08:24:52.174Z | 82.835° E | 29.773° | 2025-09-19 08:31:52.174Z | 24.552° NE |
| 14 mins | 2025-09-19 10:12:52.174Z | 217.065° SW | 2025-09-19 10:18:52.174Z | 279.788° WNW | 36.183° | 2025-09-19 10:26:52.174Z | 356.517° N |
| 5 mins | 2025-09-19 18:20:52.174Z | 45.988° ENE | 2025-09-19 18:22:52.174Z | 61.038° ENE | 12.424° | 2025-09-19 18:25:52.174Z | 82.826° E |
| 15 mins | 2025-09-19 20:11:52.174Z | 358.285° N | 2025-09-19 20:18:52.174Z | 75.109° E | 43.236° | 2025-09-19 20:26:52.174Z | 163.687° S |
| 10 mins | 2025-09-19 22:07:52.174Z | 320.483° NNW | 2025-09-19 22:12:52.174Z | 278.688° WNW | 21.246° | 2025-09-19 22:17:52.174Z | 237.219° 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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