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 30961U 99025BBB 24249.31254893 .00009915 00000-0 20051-2 0 9994
2 30961 98.9422 282.5292 0129060 227.3927 131.6327 14.56385655581819
| Epoch (UTC): | 05 September 2024 07:30:04 |
| Eccentricity: | 0.0129060 |
| inclination: | 98.9422° |
| perigee height: | 613 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 282.5292° |
| argument of perigee: | 227.3927° |
| revolutions per day: | 14.56385655 |
| mean anomaly at epoch: | 131.6327° |
| orbit number at epoch: | 58181 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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