COSMOS 1827, 17582
Orbit data source: Space-Track
COSMOS 1827, 17582 is a payload satellite owned by UNKS (CIS) in LEO that was launched on Fri, 13 Mar 1987 UTC via a TSIKLON-3 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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17582 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 COSMOS 1827
1 17582U 87026A 25260.78764285 .00000014 00000-0 15503-4 0 9991
2 17582 82.5749 6.9735 0012811 60.1891 300.0474 12.65006285778205
TLE epoch observation values (Epoch: 2025-09-17T18:54:12.342Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #26 in the year 1987 (1987-03-13 UTC)
COSMOS 1827 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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14 mins | 2025-09-19 07:03:27.737Z | 158.545° S | 2025-09-19 07:10:27.737Z | 93.858° ESE | 36.731° | 2025-09-19 07:17:27.737Z | 21.077° NNE |
13 mins | 2025-09-19 08:59:27.737Z | 230.125° WSW | 2025-09-19 09:05:27.737Z | 285.947° WNW | 29.375° | 2025-09-19 09:12:27.737Z | 349.28° N |
9 mins | 2025-09-19 17:05:27.737Z | 29.658° NE | 2025-09-19 17:09:27.737Z | 61.825° ENE | 17.606° | 2025-09-19 17:14:27.737Z | 101.58° ESE |
15 mins | 2025-09-19 18:58:27.737Z | 351.529° N | 2025-09-19 19:05:27.737Z | 290.05° WNW | 44.944° | 2025-09-19 19:13:27.737Z | 176.583° S |
6 mins | 2025-09-19 20:56:27.737Z | 303.125° NW | 2025-09-19 20:59:27.737Z | 279.22° WNW | 14.803° | 2025-09-19 21:02:27.737Z | 256.382° W |
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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