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 07530U 74089B 25344.91180769 -.00000036 00000-0 64193-4 0 9999
2 07530 101.9967 351.1603 0012357 130.0571 345.5215 12.53694099336920
| Epoch (UTC): | 10 December 2025 21:53:00 |
| Eccentricity: | 0.0012357 |
| inclination: | 101.9967° |
| perigee height: | 1439 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 351.1603° |
| argument of perigee: | 130.0571° |
| revolutions per day: | 12.53694099 |
| mean anomaly at epoch: | 345.5215° |
| orbit number at epoch: | 33692 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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