COSMOS 1579, 15085
Orbit data source: Space-Track
COSMOS 1579, 15085 is a payload satellite owned by VMF (CIS) in LEO that was launched on Fri, 29 Jun 1984 UTC via a TSIKLON-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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15085 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 COSMOS 1579
1 15085U 84069A 25260.87396759 -.00000053 00000-0 30674-4 0 9998
2 15085 65.0498 70.4923 0035995 140.9526 219.4145 13.86199638 88035
TLE epoch observation values (Epoch: 2025-09-17T20:58:30.799Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #69 in the year 1984 (1984-06-29 UTC)
COSMOS 1579 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. |
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5 mins | 2025-09-18 20:00:41.582Z | 8.708° NNE | 2025-09-18 20:02:41.582Z | 29.848° NE | 14.762° | 2025-09-18 20:05:41.582Z | 62.42° ENE |
10 mins | 2025-09-18 21:46:41.582Z | 335.093° NNW | 2025-09-18 21:51:41.582Z | 82.339° E | 42.769° | 2025-09-18 21:56:41.582Z | 139.431° SSE |
5 mins | 2025-09-18 23:35:41.582Z | 277.177° WNW | 2025-09-18 23:37:41.582Z | 253.324° W | 17.439° | 2025-09-18 23:40:41.582Z | 219.71° SW |
10 mins | 2025-09-19 12:56:41.582Z | 209.263° SW | 2025-09-19 13:00:41.582Z | 200.427° SSW | 44.834° | 2025-09-19 13:06:41.582Z | 31.883° NE |
7 mins | 2025-09-19 14:45:41.582Z | 285.575° WNW | 2025-09-19 14:48:41.582Z | 319.681° NNW | 18.57° | 2025-09-19 14:52:41.582Z | 2.895° 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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