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 25893U 99045B 25342.20402735 .00000113 00000-0 98290-4 0 9990
2 25893 82.9271 239.5594 0029951 77.3070 33.8086 13.76825514320617
| Epoch (UTC): | 08 December 2025 04:53:47 |
| Eccentricity: | 0.0029951 |
| inclination: | 82.9271° |
| perigee height: | 953 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 239.5594° |
| argument of perigee: | 77.3070° |
| revolutions per day: | 13.76825514 |
| mean anomaly at epoch: | 33.8086° |
| orbit number at epoch: | 32061 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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