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 46601U 18079BZ 25133.00188518 -.00000081 00000-0 00000-0 0 9997
2 46601 12.5694 71.0646 4516856 252.3444 54.6382 1.85741398 34066
| Epoch (UTC): | 13 May 2025 00:02:42 |
| Eccentricity: | 0.4516856 |
| inclination: | 12.5694° |
| perigee height: | 8950 km |
| apogee height: | 34203 km |
| right ascension of ascending node: | 71.0646° |
| argument of perigee: | 252.3444° |
| revolutions per day: | 1.85741398 |
| mean anomaly at epoch: | 54.6382° |
| orbit number at epoch: | 3406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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