COSMOS 1560, 14999
Orbit data source: Space-Track
COSMOS 1560, 14999 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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14999 intel report (Beta)
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Edit Public Description
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
Unknown
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 1560
1 14999U 84052B 25311.95621094 .00000002 00000-0 12563-3 0 9991
2 14999 74.0154 34.2081 0014018 346.3399 192.0214 12.46113998885277Epoch: 2025-11-07T22:56Z
TLE epoch observation values (Epoch: 2025-11-07T22:56:56.625Z)
Latitude
1.51514°
Longitude
-177.85258°
Altitude
1,493.759 km
Speed
7.113 km/s
True Right ascension
14h 15m 06s
True Declination
1° 30' 25"
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
08:31:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,489.646 km
Perigee altitude
1,467.618 km
Semi-major axis
7,856.769 km
Eccentricity
0.0014
Inclination
74.0154°
RAAN
34.2081°
Arg. of periapsis
346.3399°
True anomaly
191.988°
Mean anomaly
192.0214°
Eccentric anomaly
192.00469°
Mean motion
3.11657 °/min
Orbital period
115.51 mins
BSTAR
0.00012563
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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 1560 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 | 2025-11-08 15:55:26.652Z | 354.692° N | 2025-11-08 16:02:26.652Z | 55.02° ENE | 33.882° | 2025-11-08 16:10:26.652Z | 128.722° SE |
| 14 mins | 2025-11-08 17:54:26.652Z | 323.352° NNW | 2025-11-08 18:00:26.652Z | 266.689° W | 34.857° | 2025-11-08 18:08:26.652Z | 194.411° SSW |
| 9 mins | 2025-11-09 04:57:26.652Z | 122.702° SE | 2025-11-09 05:01:26.652Z | 91.454° ESE | 18.429° | 2025-11-09 05:06:26.652Z | 53.462° ENE |
| 15 mins | 2025-11-09 06:51:26.652Z | 201.425° SSW | 2025-11-09 06:58:26.652Z | 297.353° NW | 44.768° | 2025-11-09 07:06:26.652Z | 17.464° NNE |
| 10 mins | 2025-11-09 08:53:26.652Z | 277.533° WNW | 2025-11-09 08:57:26.652Z | 308.612° NW | 18.314° | 2025-11-09 09:03:26.652Z | 353.387° N |
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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