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 25342.85385226 .00040832 00000-0 34988-1 0 9990
2 59588 97.2718 299.3276 0077914 347.2520 12.6669 13.85213316 81608
| Epoch (UTC): | 08 December 2025 20:29:32 |
| Eccentricity: | 0.0077914 |
| inclination: | 97.2718° |
| perigee height: | 888 km |
| apogee height: | 1002 km |
| right ascension of ascending node: | 299.3276° |
| argument of perigee: | 347.2520° |
| revolutions per day: | 13.85213316 |
| mean anomaly at epoch: | 12.6669° |
| orbit number at epoch: | 8160 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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