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 29507U 06046C 24282.38582646 .00045432 00000-0 27680-2 0 9992
2 29507 97.6318 317.8474 0037302 249.6854 110.0364 15.09632741981838
| Epoch (UTC): | 08 October 2024 09:15:35 |
| Eccentricity: | 0.0037302 |
| inclination: | 97.6318° |
| perigee height: | 511 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 317.8474° |
| argument of perigee: | 249.6854° |
| revolutions per day: | 15.09632741 |
| mean anomaly at epoch: | 110.0364° |
| orbit number at epoch: | 98183 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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