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 22139.55721058 .00003784 00000-0 19117-3 0 9996
2 39679 51.6149 90.5110 0164955 217.6786 141.2539 15.08539302445076
| Epoch (UTC): | 19 May 2022 13:22:22 |
| Eccentricity: | 0.0164955 |
| inclination: | 51.6149° |
| perigee height: | 426 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 90.5110° |
| argument of perigee: | 217.6786° |
| revolutions per day: | 15.08539302 |
| mean anomaly at epoch: | 141.2539° |
| orbit number at epoch: | 44507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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