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 23341.43276031 .00000038 00000-0 76979-4 0 9990
2 24278 98.5566 296.5725 0349730 327.8081 30.2128 13.53165943348365
| Epoch (UTC): | 07 December 2023 10:23:10 |
| Eccentricity: | 0.0349730 |
| inclination: | 98.5566° |
| perigee height: | 800 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 296.5725° |
| argument of perigee: | 327.8081° |
| revolutions per day: | 13.53165943 |
| mean anomaly at epoch: | 30.2128° |
| orbit number at epoch: | 34836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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