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 24278U 96046B 24340.58208995 .00000050 00000-0 83545-4 0 9991
2 24278 98.5875 252.7978 0350954 104.3186 259.7183 13.53223992397616
| Epoch (UTC): | 05 December 2024 13:58:12 |
| Eccentricity: | 0.0350954 |
| inclination: | 98.5875° |
| perigee height: | 799 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 252.7978° |
| argument of perigee: | 104.3186° |
| revolutions per day: | 13.53223992 |
| mean anomaly at epoch: | 259.7183° |
| orbit number at epoch: | 39761 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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