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 25197.71435833 .00000837 00000-0 49634-3 0 9993
2 00012 32.8998 327.0702 1647461 129.1995 246.6827 11.47793384492759
| Epoch (UTC): | 16 July 2025 17:08:40 |
| Eccentricity: | 0.1647461 |
| inclination: | 32.8998° |
| perigee height: | 556 km |
| apogee height: | 3291 km |
| right ascension of ascending node: | 327.0702° |
| argument of perigee: | 129.1995° |
| revolutions per day: | 11.47793384 |
| mean anomaly at epoch: | 246.6827° |
| orbit number at epoch: | 49275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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