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 36416U 10009D 25080.68418305 .00001211 00000-0 29829-3 0 9998
2 36416 63.3949 193.0902 0658929 0.3795 359.7614 13.71913788752662
| Epoch (UTC): | 21 March 2025 16:25:13 |
| Eccentricity: | 0.0658929 |
| inclination: | 63.3949° |
| perigee height: | 507 km |
| apogee height: | 1478 km |
| right ascension of ascending node: | 193.0902° |
| argument of perigee: | 0.3795° |
| revolutions per day: | 13.71913788 |
| mean anomaly at epoch: | 359.7614° |
| orbit number at epoch: | 75266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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