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 00020U 59007A 24357.48198266 .00001460 00000-0 59571-3 0 9999
2 00020 33.3434 54.7162 1644752 33.2134 336.1651 11.60267542421639
| Epoch (UTC): | 22 December 2024 11:34:03 |
| Eccentricity: | 0.1644752 |
| inclination: | 33.3434° |
| perigee height: | 508 km |
| apogee height: | 3219 km |
| right ascension of ascending node: | 54.7162° |
| argument of perigee: | 33.2134° |
| revolutions per day: | 11.60267542 |
| mean anomaly at epoch: | 336.1651° |
| orbit number at epoch: | 42163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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