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 39679U 14021B 22147.44035931 .00001698 00000-0 95475-4 0 9995
2 39679 51.6166 53.8092 0164645 245.1518 113.2256 15.08588490446260
| Epoch (UTC): | 27 May 2022 10:34:07 |
| Eccentricity: | 0.0164645 |
| inclination: | 51.6166° |
| perigee height: | 426 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 53.8092° |
| argument of perigee: | 245.1518° |
| revolutions per day: | 15.08588490 |
| mean anomaly at epoch: | 113.2256° |
| orbit number at epoch: | 44626 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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