COSMOS 2502, 40358
Orbit data source: Space-Track
COSMOS 2502, 40358 is a payload satellite owned by VVKO (CIS) in LEO that was launched on Thu, 25 Dec 2014 UTC via a SOYUZ-2-1B 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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40358 intel report (Beta)
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TLE from 3 hours ago
0 COSMOS 2502
1 40358U 14086A 25199.85214601 -.00000019 00000-0 40185-4 0 9995
2 40358 67.1520 98.7938 0004802 251.6381 108.4182 13.97762634539073
TLE epoch observation values (Epoch: 2025-07-18T20:27:05.415Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #86 in the year 2014 (2014-12-25 UTC)
COSMOS 2502 Visibility forecast
Observer location: undefined°, undefined°
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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4 mins | 2025-07-19 02:08:28.195Z | 17.898° NNE | 2025-07-19 02:10:28.195Z | 38.441° NE | 12.26° | 2025-07-19 02:12:28.195Z | 58.747° ENE |
9 mins | 2025-07-19 03:53:28.195Z | 343.319° N | 2025-07-19 03:57:28.195Z | 57.822° ENE | 41.152° | 2025-07-19 04:02:28.195Z | 136.609° SSE |
6 mins | 2025-07-19 05:40:28.195Z | 284.369° WNW | 2025-07-19 05:42:28.195Z | 259.756° W | 19.116° | 2025-07-19 05:46:28.195Z | 213.823° SW |
10 mins | 2025-07-19 18:54:28.195Z | 208.089° SW | 2025-07-19 18:59:28.195Z | 9.767° NNE | 44.784° | 2025-07-19 19:04:28.195Z | 27.948° NE |
6 mins | 2025-07-19 20:43:28.195Z | 289.699° WNW | 2025-07-19 20:45:28.195Z | 312.145° NW | 16.323° | 2025-07-19 20:49:28.195Z | 355.668° 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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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