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 29528U 06051C 24275.39041035 .00000079 00000-0 56515-4 0 9995
2 29528 51.0980 145.0651 6052199 295.8592 326.7245 3.64284972238158
| Epoch (UTC): | 01 October 2024 09:22:11 |
| Eccentricity: | 0.6052199 |
| inclination: | 51.0980° |
| perigee height: | 665 km |
| apogee height: | 22262 km |
| right ascension of ascending node: | 145.0651° |
| argument of perigee: | 295.8592° |
| revolutions per day: | 3.64284972 |
| mean anomaly at epoch: | 326.7245° |
| orbit number at epoch: | 23815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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