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 22220U 92076B 23150.80301762 .00000060 00000-0 54233-4 0 9997
2 22220 70.9984 163.5940 0013850 209.5423 323.0522 14.16565144578236
| Epoch (UTC): | 30 May 2023 19:16:20 |
| Eccentricity: | 0.0013850 |
| inclination: | 70.9984° |
| perigee height: | 827 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 163.5940° |
| argument of perigee: | 209.5423° |
| revolutions per day: | 14.16565144 |
| mean anomaly at epoch: | 323.0522° |
| orbit number at epoch: | 57823 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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