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 5435U 71071A 25163.55201140 .00000519 00000-0 14094-3 0 9994
2 5435 50.1401 270.5992 0103374 266.0430 92.8677 14.59433803842646
| Epoch (UTC): | 12 June 2025 13:14:53 |
| Eccentricity: | 0.0103374 |
| inclination: | 50.1401° |
| perigee height: | 622 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 270.5992° |
| argument of perigee: | 266.0430° |
| revolutions per day: | 14.59433803 |
| mean anomaly at epoch: | 92.8677° |
| orbit number at epoch: | 84264 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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