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 30829U 99025AVP 24357.44816924 .00001231 00000-0 74629-3 0 9994
2 30829 98.7590 354.0678 0035270 255.4318 104.2938 14.07891473914320
| Epoch (UTC): | 22 December 2024 10:45:21 |
| Eccentricity: | 0.0035270 |
| inclination: | 98.7590° |
| perigee height: | 841 km |
| apogee height: | 892 km |
| right ascension of ascending node: | 354.0678° |
| argument of perigee: | 255.4318° |
| revolutions per day: | 14.07891473 |
| mean anomaly at epoch: | 104.2938° |
| orbit number at epoch: | 91432 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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