CE-SAT 1, 42769 (Decayed)
Orbit data source: Space-Track
CE-SAT 1, 42769 was a payload satellite owned by Canon STL (JP) in LEO that was launched on Fri, 23 Jun 2017 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). 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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42769 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
Canon STL
Mission
Decayed Commercial Imaging
Bus & Motor
CE-SAT, Unknown motor
Mass
65 kg wet, 65 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.5 m
Radar Cross Section
0.575 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 CE-SAT 1
1 42769U 17036E 25137.02325815 .08507654 24121-5 13397-3 0 9995
2 42769 97.0675 164.9752 0009951 244.4454 115.5822 16.47907954440542Epoch: 2025-05-17T00:33Z
TLE epoch observation values (Epoch: 2025-05-17T00:33:29.504Z)
Latitude
-0.00003°
Longitude
-78.36826°
Altitude
150.931 km
Speed
7.814 km/s
True Right ascension
10h 59m 54s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:38:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
148.121 km
Perigee altitude
135.145 km
Semi-major axis
6,519.77 km
Eccentricity
0.001
Inclination
97.0675°
RAAN
164.9752°
Arg. of periapsis
244.4454°
True anomaly
115.685°
Mean anomaly
115.5822°
Eccentric anomaly
115.6336°
Mean motion
4.12282 °/min
Orbital period
87.32 mins
BSTAR
0.00013397
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Other satellites on launch #36 in the year 2017 (2017-06-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CE-SAT 1 Visibility
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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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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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