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 data is extracted from the following two-line orbital elements,
1 24297U 96051A 25189.51256477 .00000199 00000-0 13008-3 0 9991
2 24297 70.9065 338.6468 0022001 111.0112 249.3365 14.13764336487721
| Epoch (UTC): | 08 July 2025 12:18:05 |
| Eccentricity: | 0.0022001 |
| inclination: | 70.9065° |
| perigee height: | 830 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 338.6468° |
| argument of perigee: | 111.0112° |
| revolutions per day: | 14.13764336 |
| mean anomaly at epoch: | 249.3365° |
| orbit number at epoch: | 48772 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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