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 25193.88933860 -.00000013 00000-0 -28977-4 0 9992
2 25893 82.9269 350.0300 0029663 130.3117 33.4797 13.76793616300205
| Epoch (UTC): | 12 July 2025 21:20:38 |
| Eccentricity: | 0.0029663 |
| inclination: | 82.9269° |
| perigee height: | 953 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 350.0300° |
| argument of perigee: | 130.3117° |
| revolutions per day: | 13.76793616 |
| mean anomaly at epoch: | 33.4797° |
| orbit number at epoch: | 30020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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