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 20466U 90010B 25196.92598516 .00000350 00000-0 39717-4 0 9995
2 20466 82.5037 129.7094 0020042 4.9058 355.2349 14.83281080893388
| Epoch (UTC): | 15 July 2025 22:13:25 |
| Eccentricity: | 0.0020042 |
| inclination: | 82.5037° |
| perigee height: | 605 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 129.7094° |
| argument of perigee: | 4.9058° |
| revolutions per day: | 14.83281080 |
| mean anomaly at epoch: | 355.2349° |
| orbit number at epoch: | 89338 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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