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 30679U 99025AQM 24356.77757412 .00001234 00000-0 11232-2 0 9991
2 30679 99.4209 45.0780 0172071 296.9637 129.2935 13.78982117896128
| Epoch (UTC): | 21 December 2024 18:39:42 |
| Eccentricity: | 0.0172071 |
| inclination: | 99.4209° |
| perigee height: | 841 km |
| apogee height: | 1094 km |
| right ascension of ascending node: | 45.0780° |
| argument of perigee: | 296.9637° |
| revolutions per day: | 13.78982117 |
| mean anomaly at epoch: | 129.2935° |
| orbit number at epoch: | 89612 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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