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 00012U 59001B 25190.75407629 .00000662 00000-0 39840-3 0 9996
2 00012 32.9002 351.5638 1647728 92.3818 286.5520 11.47781944491950
| Epoch (UTC): | 09 July 2025 18:05:52 |
| Eccentricity: | 0.1647728 |
| inclination: | 32.9002° |
| perigee height: | 555 km |
| apogee height: | 3291 km |
| right ascension of ascending node: | 351.5638° |
| argument of perigee: | 92.3818° |
| revolutions per day: | 11.47781944 |
| mean anomaly at epoch: | 286.5520° |
| orbit number at epoch: | 49195 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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