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 30579U 99025ALV 24357.60514918 .00001049 00000-0 67312-3 0 9990
2 30579 98.8431 25.9193 0053213 19.0391 107.5541 14.04714720915115
| Epoch (UTC): | 22 December 2024 14:31:24 |
| Eccentricity: | 0.0053213 |
| inclination: | 98.8431° |
| perigee height: | 839 km |
| apogee height: | 916 km |
| right ascension of ascending node: | 25.9193° |
| argument of perigee: | 19.0391° |
| revolutions per day: | 14.04714720 |
| mean anomaly at epoch: | 107.5541° |
| orbit number at epoch: | 91511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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