CE-SAT 1, 42769
Orbit data source: Space-Track
CE-SAT 1, 42769 is a payload satellite owned by Canon STL (JP) in SSO that was launched on Fri, 23 Jun 2017 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). 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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42769 intel report (Beta)
CE-SAT 1 details
Identifier | |
Orbit | SSO |
Last TLE update | 12 hours ago |
Origin | |
Manufacturer | Canon STL |
Mission | Operational Commercial Imaging |
Bus & Motor | CE-SAT, Unknown motor |
Mass | 65 kg wet, 65 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Box, 0.9 m |
Radar Cross Section | 0.575 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 12 hours ago
0 CE-SAT 1
1 42769U 17036E 24361.20681512 .00073144 00000-0 82486-3 0 9996
2 42769 97.1073 18.6976 0003321 236.7640 123.3301 15.62282736418133
Epoch: 2024-12-26T04:57Z
Definitive object data (Epoch: 2024-12-26T04:57:48.826Z)
Latitude | 0.00001° |
Longitude | -150.94537° |
Altitude | 385.455 km |
Speed | 7.678 km/s |
True Right ascension | 01h 14m 47s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -30.37081° |
Longitude | -146.26937° |
Altitude | 392.564 km |
Speed | 7.673 km/s |
Apparent Right ascension | 02h 53m 37s |
Apparent Declination | -36° 52' 49" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 16:30:08 |
Azimuth | 88.579° E |
Elevation | -70.907° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 380.206 km |
Perigee altitude | 375.718 km |
Semi-major axis | 6,756.099 km |
Eccentricity | 0.0003321 |
Inclination | 97.1073° |
RAAN | 18.6976° |
Arg. of periapsis | 236.764° |
True anomaly | 123.36189° |
Mean anomaly | 123.3301° |
Eccentric anomaly | 123.346° |
Mean motion | 3.9084 °/min |
BSTAR | 0.00082486 |
Orbital period | 92.11 mins |
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Other satellites on launch #36 in the year 2017 (2017-06-23 UTC)
CE-SAT 1 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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5 mins | 2024-12-27 01:04:51.593Z | 140.33° SSE | 2024-12-27 01:07:51.593Z | 51.084° ENE | 28.363° | 2024-12-27 01:09:51.593Z | 8.593° NNE |
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