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 25312.49501389 .00020946 00000-0 18888-1 0 9992
2 59588 97.3199 275.6930 0047383 28.8276 331.5487 13.83299388 77408
| Epoch (UTC): | 08 November 2025 11:52:49 |
| Eccentricity: | 0.0047383 |
| inclination: | 97.3199° |
| perigee height: | 917 km |
| apogee height: | 987 km |
| right ascension of ascending node: | 275.6930° |
| argument of perigee: | 28.8276° |
| revolutions per day: | 13.83299388 |
| mean anomaly at epoch: | 331.5487° |
| orbit number at epoch: | 7740 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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