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 25191.54412196 -.00000007 00000-0 -22655-4 0 9997
2 25893 82.9268 351.7767 0029564 136.6488 289.7374 13.76793790299880
| Epoch (UTC): | 10 July 2025 13:03:32 |
| Eccentricity: | 0.0029564 |
| inclination: | 82.9268° |
| perigee height: | 953 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 351.7767° |
| argument of perigee: | 136.6488° |
| revolutions per day: | 13.76793790 |
| mean anomaly at epoch: | 289.7374° |
| orbit number at epoch: | 29988 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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