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: 6 hours ago
TLE from 6 hours ago
0 COSMOS 1913
1 18792U 88002E 25312.15181889 .00000048 00000-0 19895-3 0 9996
2 18792 82.6026 358.1877 0013212 207.0519 207.0946 12.65740299746791Epoch: 2025-11-08T03:38Z
TLE epoch observation values (Epoch: 2025-11-08T03:38:37.152Z)
Latitude
53.51657°
Longitude
-93.99165°
Altitude
1,417.194 km
Speed
7.153 km/s
True Right ascension
00h 32m 59s
True Declination
53° 21' 57"
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
06:14:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,406.928 km
Perigee altitude
1,386.383 km
Semi-major axis
7,774.793 km
Eccentricity
0.00132
Inclination
82.6026°
RAAN
358.1877°
Arg. of periapsis
207.0519°
True anomaly
207.02575°
Mean anomaly
207.0946°
Eccentric anomaly
207.06016°
Mean motion
3.16599 °/min
Orbital period
113.71 mins
BSTAR
0.00019895
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-08 13:27:46.654Z | 21.813° NNE | 2025-11-08 13:32:46.654Z | 61.981° ENE | 20.349° | 2025-11-08 13:38:46.654Z | 111.326° ESE |
| 15 mins | 2025-11-08 15:21:46.654Z | 348.197° N | 2025-11-08 15:28:46.654Z | 262.692° W | 44.067° | 2025-11-08 15:36:46.654Z | 182.68° SSW |
| 10 mins | 2025-11-09 02:15:46.654Z | 117.162° SE | 2025-11-09 02:20:46.654Z | 75.9° E | 19.275° | 2025-11-09 02:25:46.654Z | 37.647° NE |
| 15 mins | 2025-11-09 04:06:46.654Z | 193.084° SSW | 2025-11-09 04:13:46.654Z | 257.325° W | 44.104° | 2025-11-09 04:21:46.654Z | 4.269° NNE |
| 6 mins | 2025-11-09 06:07:46.654Z | 280.18° WNW | 2025-11-09 06:09:46.654Z | 295.526° NW | 13.853° | 2025-11-09 06:13:46.654Z | 325.791° NNW |
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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