COSMOS 1562, 15001
Orbit data source: Space-Track
COSMOS 1562, 15001 is a payload satellite owned by GUKOS (CIS) in LEO that was launched on Mon, 28 May 1984 UTC via a KOSMOS 11K65M 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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15001 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Defense Communications
Bus & Motor
STRELA-1 11F625, Unknown motor
Mass
60 kg wet, 60 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Sphere, 0.4 m
Radar Cross Section
0.588 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 1562
1 15001U 84052D 25258.62034473 -.00000017 00000-0 -42928-5 0 9997
2 15001 74.0144 321.4321 0014913 177.6314 294.6943 12.49960090884470Epoch: 2025-09-15T14:53Z
TLE epoch observation values (Epoch: 2025-09-15T14:53:17.784Z)
Latitude
62.99864°
Longitude
-110.73168°
Altitude
1,470.243 km
Speed
7.136 km/s
True Right ascension
07h 09m 39s
True Declination
62° 52' 19"
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
15:49:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,474.191 km
Perigee altitude
1,450.805 km
Semi-major axis
7,840.635 km
Eccentricity
0.00149
Inclination
74.0144°
RAAN
321.4321°
Arg. of periapsis
177.6314°
True anomaly
294.53892°
Mean anomaly
294.6943°
Eccentric anomaly
294.61662°
Mean motion
3.1262 °/min
Orbital period
115.16 mins
BSTAR
-0.0000042928
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Other satellites on launch #52 in the year 1984 (1984-05-28 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 1562 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 | 2025-09-16 03:50:43.232Z | 135.646° SSE | 2025-09-16 03:56:43.232Z | 88.985° E | 21.012° | 2025-09-16 04:01:43.232Z | 50.146° ENE |
| 16 mins | 2025-09-16 05:45:43.232Z | 206.478° SW | 2025-09-16 05:52:43.232Z | 271.499° WNW | 43.831° | 2025-09-16 06:01:43.232Z | 16.164° NNE |
| 8 mins | 2025-09-16 07:48:43.232Z | 285.773° WNW | 2025-09-16 07:52:43.232Z | 316.798° NNW | 16.497° | 2025-09-16 07:56:43.232Z | 346.447° N |
| 12 mins | 2025-09-16 13:55:43.232Z | 4.747° NNE | 2025-09-16 14:01:43.232Z | 54.638° ENE | 23.967° | 2025-09-16 14:07:43.232Z | 104.017° ESE |
| 15 mins | 2025-09-16 15:52:43.232Z | 336.059° NNW | 2025-09-16 15:59:43.232Z | 272.361° WNW | 43.552° | 2025-09-16 16:07:43.232Z | 173.77° S |
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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