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 25199.99175642 .00000003 00000-0 -12333-4 0 9993
2 25893 82.9276 345.4850 0029865 113.9335 39.1591 13.76793539301035
| Epoch (UTC): | 18 July 2025 23:48:07 |
| Eccentricity: | 0.0029865 |
| inclination: | 82.9276° |
| perigee height: | 953 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 345.4850° |
| argument of perigee: | 113.9335° |
| revolutions per day: | 13.76793539 |
| mean anomaly at epoch: | 39.1591° |
| orbit number at epoch: | 30103 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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