COSMOS 1563, 15002
Orbit data source: Space-Track
COSMOS 1563, 15002 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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15002 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: 12 hours ago
TLE from 12 hours ago
0 COSMOS 1563
1 15002U 84052E 25258.46090036 .00000004 00000-0 12779-3 0 9990
2 15002 74.0087 251.0660 0023667 84.2894 71.7190 12.51834375619825Epoch: 2025-09-15T11:03Z
TLE epoch observation values (Epoch: 2025-09-15T11:03:41.791Z)
Latitude
22.78463°
Longitude
-96.40306°
Altitude
1,453.323 km
Speed
7.14 km/s
True Right ascension
04h 16m 44s
True Declination
22° 40' 23"
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
15:46:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,473.204 km
Perigee altitude
1,436.128 km
Semi-major axis
7,832.803 km
Eccentricity
0.00237
Inclination
74.0087°
RAAN
251.066°
Arg. of periapsis
84.2894°
True anomaly
71.97675°
Mean anomaly
71.719°
Eccentric anomaly
71.84785°
Mean motion
3.13089 °/min
Orbital period
114.98 mins
BSTAR
0.00012779
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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 1563 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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2025-09-15 23:44:13.467Z | 161.363° S | 2025-09-15 23:52:13.467Z | 92.623° ESE | 31.715° | 2025-09-15 23:59:13.467Z | 34.915° NE |
| 15 mins | 2025-09-16 01:42:13.467Z | 228.549° WSW | 2025-09-16 01:49:13.467Z | 299.775° NW | 36.103° | 2025-09-16 01:57:13.467Z | 9.293° NNE |
| 15 mins | 2025-09-16 09:49:13.467Z | 352.802° N | 2025-09-16 09:57:13.467Z | 61.979° ENE | 33.129° | 2025-09-16 10:04:13.467Z | 126.161° SE |
| 14 mins | 2025-09-16 11:48:13.467Z | 324.24° NNW | 2025-09-16 11:54:13.467Z | 267.121° W | 35.136° | 2025-09-16 12:02:13.467Z | 193.099° SSW |
| 8 mins | 2025-09-16 22:49:13.467Z | 115.527° SE | 2025-09-16 22:52:13.467Z | 92.144° ESE | 16.59° | 2025-09-16 22:57:13.467Z | 54.727° ENE |
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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