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 24259.69337102 .00000119 00000-0 15976-3 0 9993
2 24278 98.5796 182.4802 0349328 313.9856 43.2962 13.53210263386670
| Epoch (UTC): | 15 September 2024 16:38:27 |
| Eccentricity: | 0.0349328 |
| inclination: | 98.5796° |
| perigee height: | 800 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 182.4802° |
| argument of perigee: | 313.9856° |
| revolutions per day: | 13.53210263 |
| mean anomaly at epoch: | 43.2962° |
| orbit number at epoch: | 38667 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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