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 24357.67902918 -.00000130 00000-0 -41408-4 0 9994
2 25407 71.0119 31.0495 0008816 323.8421 36.2105 14.16091001364527
| Epoch (UTC): | 22 December 2024 16:17:48 |
| Eccentricity: | 0.0008816 |
| inclination: | 71.0119° |
| perigee height: | 832 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 31.0495° |
| argument of perigee: | 323.8421° |
| revolutions per day: | 14.16091001 |
| mean anomaly at epoch: | 36.2105° |
| orbit number at epoch: | 36452 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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