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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Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Spacecraft
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
POLY, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 COSMOS 1562
1 15001U 84052D 26277.45354650 -.00000021 00000-0 -29744-4 0 9997
2 15001 74.0133 170.8515 0015563 316.9953 219.1305 12.49966969932433Epoch: 2026-10-04T10:53Z
TLE epoch observation values (Epoch: 2026-10-04T10:53:06.417Z)
Latitude
3.75229°
Longitude
173.35686°
Altitude
1,476.081 km
Speed
7.121 km/s
True Right ascension
23h 19m 07s
True Declination
3° 43' 55"
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
18:05:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,474.672 km
Perigee altitude
1,450.267 km
Semi-major axis
7,840.606 km
Eccentricity
0.00156
Inclination
74.0133°
RAAN
170.8515°
Arg. of periapsis
316.9953°
True anomaly
219.01812°
Mean anomaly
219.1305°
Eccentric anomaly
219.07429°
Mean motion
3.12621 °/min
Orbital period
115.16 mins
BSTAR
-0.000029744
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-05 01:53:30.629Z | 13.156° NNE | 2026-10-05 01:57:30.629Z | 41.013° NE | 14.256° | 2026-10-05 02:01:30.629Z | 69.562° E |
| 15 mins | 2026-10-05 03:50:30.629Z | 350.028° N | 2026-10-05 03:57:30.629Z | 68.629° E | 61.831° | 2026-10-05 04:05:30.629Z | 145.972° SSE |
| 12 mins | 2026-10-05 05:48:30.629Z | 315.026° NNW | 2026-10-05 05:54:30.629Z | 264.486° W | 28.683° | 2026-10-05 06:00:30.629Z | 215.39° SW |
| 12 mins | 2026-10-05 16:47:30.629Z | 142.942° SSE | 2026-10-05 16:52:30.629Z | 99.615° ESE | 29.923° | 2026-10-05 16:59:30.629Z | 41.046° NE |
| 16 mins | 2026-10-05 18:42:30.629Z | 217.276° SW | 2026-10-05 18:49:30.629Z | 282.095° WNW | 58.332° | 2026-10-05 18:58:30.629Z | 12.695° NNE |
| 6 mins | 2026-10-05 20:47:30.629Z | 301.978° NW | 2026-10-05 20:49:30.629Z | 316.47° NNW | 13.454° | 2026-10-05 20:53:30.629Z | 344.52° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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