CERTIFICATE OF RE-ENTRYOrbital Register™ · by Orbital Radar™
Entry no.
2026-0774
CE-SAT IIB
CE-SAT IIB (NORAD 46818) re-entered Earth’s atmosphere on 14 July 2026, after 5 years, 8 months in orbit.
Official date
NORAD number
46818
International designator
2020-077F
Object type
Spacecraft
Country
Japan
Launched
28 Oct 2020Rocket Lab Launch Complex
Re-entered (UTC)
14 Jul 2026UTC calendar day
Time in orbit
5 years, 8 months2,085 days
How it ended
Re-entered (natural decay)
Latitude range
82.8°N to 82.8°SFinal inclination 97.2°
Mass
35 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 97.2°, allowed a re-entry anywhere between 82.8°N and 82.8°S.
Life in orbit
5 years, 8 monthsCE-SAT IIB’s lowest and highest points above Earth, week by week, from its tracking history.
Also ended on 14 Jul 2026
4 entriesFrom the same launch
2020-077
Entered in the Orbital Register™ on 7 November 2026.
Record version 1 · No corrections · orbitalradar.com/register/2026-0774
© 2026 Orbital Radar. Cite this entry by its number; the register itself may not be copied.
Record version 1 · No corrections · orbitalradar.com/register/2026-0774
© 2026 Orbital Radar. Cite this entry by its number; the register itself may not be copied.