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 25940U 99057A 25193.50369902 .00000111 00000-0 53487-4 0 9998
2 25940 98.8395 188.6230 0003819 284.0342 76.0418 14.36793376348736
| Epoch (UTC): | 12 July 2025 12:05:19 |
| Eccentricity: | 0.0003819 |
| inclination: | 98.8395° |
| perigee height: | 766 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 188.6230° |
| argument of perigee: | 284.0342° |
| revolutions per day: | 14.36793376 |
| mean anomaly at epoch: | 76.0418° |
| orbit number at epoch: | 34873 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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