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Spacecraft information: CE-SAT-IE
Launch Details
| Launched | 16 February 2024 |
| Flight ended | – |
| Status | Operational |
| Category |
Active satellites
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| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 58987 |
| COSPAR ID | 2024-032A |
| Observing |
Current orbital elements
| Inclination | 98.010° |
| Eccentricity | 0.00037 |
| RA ascending node | 8.351 hr |
| Argument perigee | 56.276° |
| Mean anomaly | 303.879° |
| Orbital period | 98.080 min |
| Epoch of osculation | 09 Mar 2026, 09:32 |
Derived Quantities
| Min Altitude | 671.4 km |
| Mean Altitude | 674.0 km |
| Peak Altitude | 676.6 km |
Orbital History
Drag the graphs below left or right to change the time range, or use your scroll wheel to zoom in or out.