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 25080.54075103 .00000046 00000-0 47506-4 0 9990
2 25407 71.0114 204.1980 0008759 217.5373 142.5140 14.16120157377108
| Epoch (UTC): | 21 March 2025 12:58:40 |
| Eccentricity: | 0.0008759 |
| inclination: | 71.0114° |
| perigee height: | 832 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 204.1980° |
| argument of perigee: | 217.5373° |
| revolutions per day: | 14.16120157 |
| mean anomaly at epoch: | 142.5140° |
| orbit number at epoch: | 37710 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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