CERTIFICATE OF RE-ENTRYOrbital Register™ · by Orbital Radar™
Entry no.
2025-1056
CE-SAT 1
CE-SAT 1 (NORAD 42769) re-entered Earth’s atmosphere on 20 May 2025, after 7 years, 10 months in orbit.
Official date
NORAD number
42769
International designator
2017-036E
Object type
Spacecraft
Country
Japan
Launched
23 Jun 2017Sriharikota
Re-entered (UTC)
20 May 2025UTC calendar day
Time in orbit
7 years, 10 months2,888 days
How it ended
Re-entered (natural decay)
Latitude range
82.9°N to 82.9°SFinal inclination 97.1°
Mass
65 kg
Operator
Canon STL
Built by
Canon STL
Bus
CE-SAT
Programme
Canon
Where it came down
Latitude band its orbit allowedExact position not recorded
No position was recorded for this re-entry. Its final orbit, inclined at 97.1°, allowed a re-entry anywhere between 82.9°N and 82.9°S.
Life in orbit
7 years, 10 monthsCE-SAT 1’s lowest and highest points above Earth, week by week, from its tracking history.
Also ended on 20 May 2025
7 entriesFrom the same launch
2017-036
Entered in the Orbital Register™, founding volume, September 2026.
Record version 1 · No corrections · orbitalradar.com/register/2025-1056
© 2026 Orbital Radar. Cite this entry by its number; the register itself may not be copied.
Record version 1 · No corrections · orbitalradar.com/register/2025-1056
© 2026 Orbital Radar. Cite this entry by its number; the register itself may not be copied.