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 22148.23528875 .00001796 00000-0 99951-4 0 9999
2 39679 51.6167 50.1083 0164621 247.9243 110.4176 15.08592797446063
| Epoch (UTC): | 28 May 2022 05:38:48 |
| Eccentricity: | 0.0164621 |
| inclination: | 51.6167° |
| perigee height: | 426 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 50.1083° |
| argument of perigee: | 247.9243° |
| revolutions per day: | 15.08592797 |
| mean anomaly at epoch: | 110.4176° |
| orbit number at epoch: | 44606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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