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 25407U 98045B 24284.42653814 .00000318 00000-0 18489-3 0 9992
2 25407 71.0114 185.0671 0005291 91.7028 268.4701 14.16053584354159
| Epoch (UTC): | 10 October 2024 10:14:12 |
| Eccentricity: | 0.0005291 |
| inclination: | 71.0114° |
| perigee height: | 835 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 185.0671° |
| argument of perigee: | 91.7028° |
| revolutions per day: | 14.16053584 |
| mean anomaly at epoch: | 268.4701° |
| orbit number at epoch: | 35415 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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