COSMOS 1564, 15003
Orbit data source: Space-Track
COSMOS 1564, 15003 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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15003 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: 17 hours ago
TLE from 17 hours ago
0 COSMOS 1564
1 15003U 84052F 25258.25388764 -.00000004 00000-0 77674-4 0 9993
2 15003 74.0137 186.0485 0032938 1.3030 153.1854 12.53579720889819Epoch: 2025-09-15T06:05Z
TLE epoch observation values (Epoch: 2025-09-15T06:05:35.892Z)
Latitude
24.32589°
Longitude
-87.21681°
Altitude
1,475.04 km
Speed
7.117 km/s
True Right ascension
23h 54m 34s
True Declination
24° 12' 32"
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
15:47:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,473.165 km
Perigee altitude
1,421.614 km
Semi-major axis
7,825.527 km
Eccentricity
0.00329
Inclination
74.0137°
RAAN
186.0485°
Arg. of periapsis
1.303°
True anomaly
153.35504°
Mean anomaly
153.1854°
Eccentric anomaly
153.27028°
Mean motion
3.13525 °/min
Orbital period
114.82 mins
BSTAR
0.000077674
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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 1564 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 | 2025-09-16 04:50:10.279Z | 4.824° NNE | 2025-09-16 04:56:10.279Z | 53.107° ENE | 22.796° | 2025-09-16 05:02:10.279Z | 101.237° ESE |
| 15 mins | 2025-09-16 06:47:10.279Z | 337.486° NNW | 2025-09-16 06:54:10.279Z | 267.372° W | 44.345° | 2025-09-16 07:02:10.279Z | 170.479° S |
| 5 mins | 2025-09-16 08:48:10.279Z | 286.624° WNW | 2025-09-16 08:50:10.279Z | 271.963° WNW | 13.26° | 2025-09-16 08:53:10.279Z | 250.644° W |
| 15 mins | 2025-09-16 19:40:10.279Z | 172.352° S | 2025-09-16 19:47:10.279Z | 100.572° ESE | 38.854° | 2025-09-16 19:55:10.279Z | 28.171° NE |
| 14 mins | 2025-09-16 21:38:10.279Z | 242.719° WSW | 2025-09-16 21:44:10.279Z | 294.828° NW | 29.357° | 2025-09-16 21:52:10.279Z | 4.287° NNE |
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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