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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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: 16 hours ago
TLE from 16 hours ago
0 COSMOS 1913
1 18792U 88002E 26092.42955017 .00000027 00000-0 89831-4 0 9999
2 18792 82.5948 265.1473 0012911 238.2174 148.1884 12.65746832765178Epoch: 2026-04-02T10:18Z
TLE epoch observation values (Epoch: 2026-04-02T10:18:33.134Z)
Latitude
26.27759°
Longitude
-76.60781°
Altitude
1,410.908 km
Speed
7.153 km/s
True Right ascension
17h 55m 14s
True Declination
26° 09' 10"
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
08:29:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,406.667 km
Perigee altitude
1,386.591 km
Semi-major axis
7,774.766 km
Eccentricity
0.00129
Inclination
82.5948°
RAAN
265.1473°
Arg. of periapsis
238.2174°
True anomaly
148.26628°
Mean anomaly
148.1884°
Eccentric anomaly
148.22735°
Mean motion
3.16601 °/min
Orbital period
113.71 mins
BSTAR
0.000089831
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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 | 2026-04-03 10:56:21.870Z | 139.456° SSE | 2026-04-03 11:02:21.870Z | 87.727° E | 27.771° | 2026-04-03 11:09:21.870Z | 27.466° NE |
| 14 mins | 2026-04-03 12:50:21.870Z | 211.968° SW | 2026-04-03 12:57:21.870Z | 293.846° NW | 38.037° | 2026-04-03 13:04:21.870Z | 357.001° N |
| 14 mins | 2026-04-03 22:50:21.870Z | 1.505° NNE | 2026-04-03 22:56:21.870Z | 62.904° ENE | 41.696° | 2026-04-03 23:04:21.870Z | 159.381° S |
| 10 mins | 2026-04-04 00:46:21.870Z | 318.204° NNW | 2026-04-04 00:50:21.870Z | 282.791° WNW | 23.008° | 2026-04-04 00:56:21.870Z | 231.216° 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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