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 29769U 99025BK 24358.08393737 .00004301 00000-0 23236-2 0 9996
2 29769 99.1334 43.2173 0094951 46.9341 313.9729 14.10872006917021
| Epoch (UTC): | 23 December 2024 02:00:52 |
| Eccentricity: | 0.0094951 |
| inclination: | 99.1334° |
| perigee height: | 788 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 43.2173° |
| argument of perigee: | 46.9341° |
| revolutions per day: | 14.10872006 |
| mean anomaly at epoch: | 313.9729° |
| orbit number at epoch: | 91702 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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