TRAAC, 205
Orbit data source: Space-Track
TRAAC, 205 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Wed, 15 Nov 1961 UTC via a THOR ABLESTAR launch vehicle from the Air Force Eastern Test Range (AFETR). 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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205 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 TRAAC
1 00205U 61031B 25260.48460249 .00000037 00000-0 20873-4 0 9994
2 00205 32.4405 81.2942 0101568 65.5216 295.5959 13.62551642181851
TLE epoch observation values (Epoch: 2025-09-17T11:37:49.655Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #31 in the year 1961 (1961-11-15 UTC)
TRAAC 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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8 mins | 2025-09-18 19:45:59.001Z | 237.499° WSW | 2025-09-18 19:48:59.001Z | 190.027° SSW | 29.544° | 2025-09-18 19:53:59.001Z | 133.771° SE |
6 mins | 2025-09-18 21:37:59.001Z | 231.649° WSW | 2025-09-18 21:39:59.001Z | 211.068° SW | 15.751° | 2025-09-18 21:43:59.001Z | 172.68° S |
8 mins | 2025-09-19 14:50:59.001Z | 197.069° SSW | 2025-09-19 14:54:59.001Z | 151.136° SSE | 20.953° | 2025-09-19 14:58:59.001Z | 109.994° ESE |
10 mins | 2025-09-19 16:41:59.001Z | 230.657° WSW | 2025-09-19 16:45:59.001Z | 175.707° S | 32.597° | 2025-09-19 16:51:59.001Z | 104.68° ESE |
9 mins | 2025-09-19 18:33:59.001Z | 245.963° WSW | 2025-09-19 18:37:59.001Z | 186.99° SSW | 33.029° | 2025-09-19 18:42:59.001Z | 123.668° SE |
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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