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 25188.56453352 -.00000009 00000-0 -24815-4 0 9996
2 25893 82.9266 353.9960 0029415 144.6949 281.8216 13.76793906299475
| Epoch (UTC): | 07 July 2025 13:32:55 |
| Eccentricity: | 0.0029415 |
| inclination: | 82.9266° |
| perigee height: | 953 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 353.9960° |
| argument of perigee: | 144.6949° |
| revolutions per day: | 13.76793906 |
| mean anomaly at epoch: | 281.8216° |
| orbit number at epoch: | 29947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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