View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 24305U 26088.20467966 +.00000000 +00000-0 +63193-4 0 00007
2 24305 82.9366 139.4189 0031528 113.7296 246.7172 13.74076562 03
| Epoch (UTC): | 29 March 2026 04:54:44 |
| Eccentricity: | 0.0031528 |
| inclination: | 82.9366° |
| perigee height: | 962 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 139.4189° |
| argument of perigee: | 113.7296° |
| revolutions per day: | 13.74076562 |
| mean anomaly at epoch: | 246.7172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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