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 24007U 26088.23791117 +.00000000 +00000-0 +32202-3 0 00003
2 24007 81.9238 349.9693 0063516 138.4061 346.5866 15.02806869 06
| Epoch (UTC): | 29 March 2026 05:42:35 |
| Eccentricity: | 0.0063516 |
| inclination: | 81.9238° |
| perigee height: | 514 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 349.9693° |
| argument of perigee: | 138.4061° |
| revolutions per day: | 15.02806869 |
| mean anomaly at epoch: | 346.5866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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