COSMOS 1691, 16139
Orbit data source: Space-Track
COSMOS 1691, 16139 is a payload satellite owned by GUKOS (CIS) in LEO that was launched on Wed, 09 Oct 1985 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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16139 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 1691
1 16139U 85094B 25260.00977139 .00000043 00000-0 18269-3 0 9993
2 16139 82.6070 103.5151 0001242 80.0192 73.3191 12.62464935840761
TLE epoch observation values (Epoch: 2025-09-17T00:14:04.248Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #94 in the year 1985 (1985-10-09 UTC)
COSMOS 1691 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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15 mins | 2025-09-18 13:33:02.982Z | 159.548° S | 2025-09-18 13:40:02.982Z | 98.951° ESE | 37.019° | 2025-09-18 13:48:02.982Z | 18.877° NNE |
13 mins | 2025-09-18 15:30:02.982Z | 233.434° WSW | 2025-09-18 15:36:02.982Z | 293.172° NW | 29.158° | 2025-09-18 15:43:02.982Z | 350.984° N |
9 mins | 2025-09-18 23:37:02.982Z | 32.795° NE | 2025-09-18 23:41:02.982Z | 66.286° ENE | 18.278° | 2025-09-18 23:46:02.982Z | 105.113° ESE |
15 mins | 2025-09-19 01:30:02.982Z | 350.843° N | 2025-09-19 01:37:02.982Z | 236.567° WSW | 44.827° | 2025-09-19 01:45:02.982Z | 177.871° S |
6 mins | 2025-09-19 03:28:02.982Z | 302.562° NW | 2025-09-19 03:30:02.982Z | 287.111° WNW | 14.313° | 2025-09-19 03:34:02.982Z | 256.755° 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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