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 25191.65086864 .00000033 00000-0 40946-4 0 9998
2 25407 71.0122 330.5574 0006489 18.7470 341.3891 14.16142541392837
| Epoch (UTC): | 10 July 2025 15:37:15 |
| Eccentricity: | 0.0006489 |
| inclination: | 71.0122° |
| perigee height: | 834 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 330.5574° |
| argument of perigee: | 18.7470° |
| revolutions per day: | 14.16142541 |
| mean anomaly at epoch: | 341.3891° |
| orbit number at epoch: | 39283 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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