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 12U 59001B 25198.58424818 .00000874 00000-0 51719-3 0 9998
2 12 32.8998 324.0088 1647437 133.8014 241.1194 11.47795099735448
| Epoch (UTC): | 17 July 2025 14:01:19 |
| Eccentricity: | 0.1647437 |
| inclination: | 32.8998° |
| perigee height: | 556 km |
| apogee height: | 3291 km |
| right ascension of ascending node: | 324.0088° |
| argument of perigee: | 133.8014° |
| revolutions per day: | 11.47795099 |
| mean anomaly at epoch: | 241.1194° |
| orbit number at epoch: | 73544 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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