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 59588U 24077B 25317.48542030 .00029134 00000-0 25994-1 0 9998
2 59588 97.3104 279.5884 0056798 25.0838 335.3063 13.83614992 78098
| Epoch (UTC): | 13 November 2025 11:39:00 |
| Eccentricity: | 0.0056798 |
| inclination: | 97.3104° |
| perigee height: | 909 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 279.5884° |
| argument of perigee: | 25.0838° |
| revolutions per day: | 13.83614992 |
| mean anomaly at epoch: | 335.3063° |
| orbit number at epoch: | 7809 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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