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 25326.05802105 .00000035 00000-0 12814-3 0 9991
2 18792 82.6005 349.2831 0013769 175.1556 213.1921 12.65741129748552Epoch: 2025-11-22T01:23Z
TLE epoch observation values (Epoch: 2025-11-22T01:23:33.018Z)
Latitude
28.0444°
Longitude
-88.94928°
Altitude
1,411.619 km
Speed
7.153 km/s
True Right ascension
23h 32m 55s
True Declination
27° 54' 50"
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
06:42:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,407.357 km
Perigee altitude
1,385.947 km
Semi-major axis
7,774.789 km
Eccentricity
0.00138
Inclination
82.6005°
RAAN
349.2831°
Arg. of periapsis
175.1556°
True anomaly
213.10585°
Mean anomaly
213.1921°
Eccentric anomaly
213.14896°
Mean motion
3.166 °/min
Orbital period
113.71 mins
BSTAR
0.00012814
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-22 11:23:02.173Z | 43.257° NE | 2025-11-22 11:25:02.173Z | 57.982° ENE | 11.54° | 2025-11-22 11:27:02.173Z | 72.769° E |
| 14 mins | 2025-11-22 13:15:02.173Z | 0.294° NNE | 2025-11-22 13:21:02.173Z | 60.088° ENE | 42.344° | 2025-11-22 13:29:02.173Z | 161.389° S |
| 10 mins | 2025-11-22 15:11:02.173Z | 317.549° NNW | 2025-11-22 15:15:02.173Z | 282.765° WNW | 21.855° | 2025-11-22 15:21:02.173Z | 232.538° WSW |
| 15 mins | 2025-11-23 02:00:02.173Z | 170.352° S | 2025-11-23 02:07:02.173Z | 90.197° ESE | 42.446° | 2025-11-23 02:15:02.173Z | 13.322° NNE |
| 11 mins | 2025-11-23 03:57:02.173Z | 246.013° WSW | 2025-11-23 04:02:02.173Z | 289.188° WNW | 23.199° | 2025-11-23 04:08:02.173Z | 340.779° 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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