CE-SAT-IE
Launch
Launched on Feb 17, 2024 from Yoshinobu Launch Complex LP-2, Japan aboard a H3-22.
H3-22 | VEP 4, CE-SAT-1E & TIRSAT →Live · TLE epoch 2026-10-23 23:07 UTC
Orbit class
SSO — Sun-Synchronous (LEO at 96–102° inclination)
Operator
JAXA
Country
Japan
Manufacturer
—
Launched
Feb 17, 2024
Mass
—
Apogee
673 km
Perigee
668 km
Inclination
97.98°
Period
1.63 h
Altitude history
Apogee and perigee for CE-SAT-IE across 59 days of archived orbital elements (60 element sets, one per day).
Trend
Stable
Change
-0.1 km
Rate
-0.00 km/day
Now
668 × 673 km
Apogee Perigee
Derived from our own archive of CelesTrak orbital elements, sampled every 3 hours. Short windows show drag and station-keeping; they are not a reentry prediction.
Launched with
One other catalogued object still in orbit from launch 2024-032 (H3-22 | VEP 4, CE-SAT-1E & TIRSAT).
- TIRSAT · 58989
Sources & further reading
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