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 24276.35355781 .00013459 00000-0 83140-3 0 9998
2 29507 97.6331 311.8431 0036918 270.9735 88.7264 15.09424591980872
| Epoch (UTC): | 02 October 2024 08:29:07 |
| Eccentricity: | 0.0036918 |
| inclination: | 97.6331° |
| perigee height: | 512 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 311.8431° |
| argument of perigee: | 270.9735° |
| revolutions per day: | 15.09424591 |
| mean anomaly at epoch: | 88.7264° |
| orbit number at epoch: | 98087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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