ORS 5 SENSORSAT, 42921
Orbit data source: Space-Track
ORS 5 SENSORSAT, 42921 is a payload satellite owned by DoD ORS (US) in LEO that was launched on Sat, 26 Aug 2017 UTC via an MINOTAUR IV launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets 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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42921 intel report (Beta)
ORS 5 SENSORSAT details
Identifier | |
Orbit | LEO |
Last TLE update | 9 hours ago |
Origin | |
Manufacturer | MIT-LL |
Mission | Operational Defense Early Warn |
Bus & Motor | ORS-5, Unknown motor |
Mass | ~110 kg wet, ~110 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Box + 2 Pan, 1.5 m |
Radar Cross Section | 1.080 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 ORS 5 SENSORSAT
1 42921U 17050A 24361.28773371 .00006148 00000-0 44309-3 0 9997
2 42921 0.0467 186.4536 0011250 337.0901 196.4928 14.97621894400714
Epoch: 2024-12-26T06:54Z
Definitive object data (Epoch: 2024-12-26T06:54:20.192Z)
Latitude | 0.00528° |
Longitude | 161.1466° |
Altitude | 578.59 km |
Speed | 7.571 km/s |
True Right ascension | 00h 00m 00s |
True Declination | 0° 00' 19" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 0.03889° |
Longitude | 108.80873° |
Altitude | 577.167 km |
Speed | 7.572 km/s |
Apparent Right ascension | 23h 11m 51s |
Apparent Declination | -29° 18' 35" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 15:38:36 |
Azimuth | 100.888° ESE |
Elevation | -35.364° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 588.418 km |
Perigee altitude | 572.761 km |
Semi-major axis | 6,958.727 km |
Eccentricity | 0.001125 |
Inclination | 0.0467° |
RAAN | 186.4536° |
Arg. of periapsis | 337.0901° |
True anomaly | 196.45625° |
Mean anomaly | 196.4928° |
Eccentric anomaly | 196.47452° |
Mean motion | 3.73894 °/min |
BSTAR | 0.00044309 |
Orbital period | 96.28 mins |
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Other satellites on launch #50 in the year 2017 (2017-08-26 UTC)
ORS 5 SENSORSAT, 42921 |
MINOTAUR DEB, 42922 (Decayed) |
MINOTAUR DEB, 42923 (Decayed) |
MINOTAUR DEB, 42924 (Decayed) |
MINOTAUR R/B, 42925 |
MINOTAUR DEB, 42926 (Decayed) |
MINOTAUR R/B, 42927 (Decayed) |
ORS 5 SENSORSAT 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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