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 24946U 26088.17925802 +.00000000 +00000-0 +11276-3 0 00006
2 24946 86.3914 23.5227 0006351 215.3090 144.7686 14.35112968 00
| Epoch (UTC): | 29 March 2026 04:18:07 |
| Eccentricity: | 0.0006351 |
| inclination: | 86.3914° |
| perigee height: | 770 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 23.5227° |
| argument of perigee: | 215.3090° |
| revolutions per day: | 14.35112968 |
| mean anomaly at epoch: | 144.7686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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