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 30708U 99025ARS 24358.01693104 .00000489 00000-0 29094-3 0 9997
2 30708 98.7110 16.1350 0009176 126.2500 263.3734 14.11876157918299
| Epoch (UTC): | 23 December 2024 00:24:22 |
| Eccentricity: | 0.0009176 |
| inclination: | 98.7110° |
| perigee height: | 846 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 16.1350° |
| argument of perigee: | 126.2500° |
| revolutions per day: | 14.11876157 |
| mean anomaly at epoch: | 263.3734° |
| orbit number at epoch: | 91829 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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