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 61936U 24208A 24358.17491507 .00001360 00000-0 21787-3 0 9995
2 61936 98.0063 2.2578 0001302 97.5618 262.5738 14.73309147 5781
| Epoch (UTC): | 23 December 2024 04:11:52 |
| Eccentricity: | 0.0001302 |
| inclination: | 98.0063° |
| perigee height: | 649 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 2.2578° |
| argument of perigee: | 97.5618° |
| revolutions per day: | 14.73309147 |
| mean anomaly at epoch: | 262.5738° |
| orbit number at epoch: | 578 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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