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 22078U 92052C 23083.63851100 -.00000056 00000-0 25145-4 0 9990
2 22078 66.0839 222.6590 0004042 171.1666 188.9424 12.86809725438714
| Epoch (UTC): | 24 March 2023 15:19:27 |
| Eccentricity: | 0.0004042 |
| inclination: | 66.0839° |
| perigee height: | 1311 km |
| apogee height: | 1317 km |
| right ascension of ascending node: | 222.6590° |
| argument of perigee: | 171.1666° |
| revolutions per day: | 12.86809725 |
| mean anomaly at epoch: | 188.9424° |
| orbit number at epoch: | 43871 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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