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 25860U 99039A 25200.07730645 .00000504 00000-0 73888-4 0 9999
2 25860 97.9815 256.8771 0001633 72.1282 288.0108 14.79844714399921
| Epoch (UTC): | 19 July 2025 01:51:19 |
| Eccentricity: | 0.0001633 |
| inclination: | 97.9815° |
| perigee height: | 628 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 256.8771° |
| argument of perigee: | 72.1282° |
| revolutions per day: | 14.79844714 |
| mean anomaly at epoch: | 288.0108° |
| orbit number at epoch: | 39992 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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