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 25305.61286565 .00000033 00000-0 11853-3 0 9996
2 18792 82.6035 2.3739 0012969 222.4383 290.8126 12.65739866745960Epoch: 2025-11-01T14:42Z
TLE epoch observation values (Epoch: 2025-11-01T14:42:31.592Z)
Latitude
26.68026°
Longitude
-83.11994°
Altitude
1,398.882 km
Speed
7.164 km/s
True Right ascension
11h 54m 36s
True Declination
26° 33' 14"
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
12:28:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,406.74 km
Perigee altitude
1,386.574 km
Semi-major axis
7,774.794 km
Eccentricity
0.0013
Inclination
82.6035°
RAAN
2.3739°
Arg. of periapsis
222.4383°
True anomaly
290.6736°
Mean anomaly
290.8126°
Eccentric anomaly
290.74311°
Mean motion
3.16599 °/min
Orbital period
113.71 mins
BSTAR
0.00011853
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-02 17:05:50.716Z | 328.388° NNW | 2025-11-02 17:11:50.716Z | 276.077° WNW | 26.1° | 2025-11-02 17:17:50.716Z | 224.037° SW |
| 14 mins | 2025-11-03 03:56:50.716Z | 160.672° S | 2025-11-03 04:02:50.716Z | 98.811° ESE | 39.103° | 2025-11-03 04:10:50.716Z | 17.014° NNE |
| 12 mins | 2025-11-03 05:52:50.716Z | 238.621° WSW | 2025-11-03 05:57:50.716Z | 284.946° WNW | 27.098° | 2025-11-03 06:04:50.716Z | 346.947° N |
| 10 mins | 2025-11-03 13:57:50.716Z | 28.878° NE | 2025-11-03 14:01:50.716Z | 62.367° ENE | 19.515° | 2025-11-03 14:07:50.716Z | 110.327° ESE |
| 15 mins | 2025-11-03 15:50:50.716Z | 349.214° N | 2025-11-03 15:57:50.716Z | 259.438° W | 44.454° | 2025-11-03 16:05:50.716Z | 180.811° 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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