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 23335.88743372 .00000079 00000-0 11758-3 0 9997
2 24278 98.5556 291.7683 0349927 342.1914 16.7210 13.53165091347619
| Epoch (UTC): | 01 December 2023 21:17:54 |
| Eccentricity: | 0.0349927 |
| inclination: | 98.5556° |
| perigee height: | 800 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 291.7683° |
| argument of perigee: | 342.1914° |
| revolutions per day: | 13.53165091 |
| mean anomaly at epoch: | 16.7210° |
| orbit number at epoch: | 34761 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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