COSMOS 1565, 15004
Orbit data source: Space-Track
COSMOS 1565, 15004 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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15004 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: 8 hours ago
TLE from 8 hours ago
0 COSMOS 1565
1 15004U 84052G 25342.47808054 -.00000004 00000-0 72287-4 0 9996
2 15004 74.0136 1.9073 0043104 155.0387 276.2279 12.55459694903214Epoch: 2025-12-08T11:28Z
TLE epoch observation values (Epoch: 2025-12-08T11:28:26.158Z)
Latitude
65.28211°
Longitude
150.58655°
Altitude
1,449.134 km
Speed
7.145 km/s
True Right ascension
02h 40m 41s
True Declination
65° 09' 46"
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
18:00:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,473.269 km
Perigee altitude
1,405.874 km
Semi-major axis
7,817.708 km
Eccentricity
0.00431
Inclination
74.0136°
RAAN
1.9073°
Arg. of periapsis
155.0387°
True anomaly
275.7366°
Mean anomaly
276.2279°
Eccentric anomaly
275.98228°
Mean motion
3.13996 °/min
Orbital period
114.65 mins
BSTAR
0.000072287
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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 1565 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-09 00:38:19.688Z | 109.363° ESE | 2025-12-09 00:41:19.688Z | 87.626° E | 13.575° | 2025-12-09 00:44:19.688Z | 65.846° ENE |
| 16 mins | 2025-12-09 02:29:19.688Z | 190.395° SSW | 2025-12-09 02:37:19.688Z | 73.163° E | 44.338° | 2025-12-09 02:45:19.688Z | 21.5° NNE |
| 12 mins | 2025-12-09 04:29:19.688Z | 261.453° W | 2025-12-09 04:35:19.688Z | 311.08° NW | 22.157° | 2025-12-09 04:41:19.688Z | 357.275° N |
| 9 mins | 2025-12-09 10:38:19.688Z | 14.451° NNE | 2025-12-09 10:42:19.688Z | 45.471° ENE | 16.8° | 2025-12-09 10:47:19.688Z | 84.056° E |
| 15 mins | 2025-12-09 12:34:19.688Z | 344.556° N | 2025-12-09 12:41:19.688Z | 85.313° E | 44.366° | 2025-12-09 12:49:19.688Z | 156.988° SSE |
| 9 mins | 2025-12-09 14:33:19.688Z | 300.785° NW | 2025-12-09 14:37:19.688Z | 267.256° W | 19.022° | 2025-12-09 14:42:19.688Z | 228.486° WSW |
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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