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 23336.84862260 .00000066 00000-0 10432-3 0 9996
2 24278 98.5558 292.6010 0349874 339.6997 19.0517 13.53165209347749
| Epoch (UTC): | 02 December 2023 20:22:00 |
| Eccentricity: | 0.0349874 |
| inclination: | 98.5558° |
| perigee height: | 800 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 292.6010° |
| argument of perigee: | 339.6997° |
| revolutions per day: | 13.53165209 |
| mean anomaly at epoch: | 19.0517° |
| orbit number at epoch: | 34774 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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