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 10490U 77108B 24277.20051194 .00002698 00000-0 66344-3 0 9992
2 10490 28.2969 315.4807 1157914 137.7548 231.8257 12.69696687150939
| Epoch (UTC): | 03 October 2024 04:48:44 |
| Eccentricity: | 0.1157914 |
| inclination: | 28.2969° |
| perigee height: | 484 km |
| apogee height: | 2282 km |
| right ascension of ascending node: | 315.4807° |
| argument of perigee: | 137.7548° |
| revolutions per day: | 12.69696687 |
| mean anomaly at epoch: | 231.8257° |
| orbit number at epoch: | 15093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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