CE-SAT-IE

NORAD 58987· COSPAR 2024-032A· Active satellite· Other / Unclassified· SSO

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 2026-09-08 09:00 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

97.99°

Period

1.63 h

Altitude history

Apogee and perigee for CE-SAT-IE across 14 days of archived orbital elements (15 element sets, one per day).

Trend

Stable

Change

-0.0 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

Embed this satellite on your site

Free for editorial use. Attribution back to LowEarth is required.

<iframe src="https://lowearth.app/embed/58987" width="640" height="400" frameborder="0" allow="fullscreen"></iframe>