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 23150.51880045 .00000079 00000-0 63350-4 0 9991
2 22220 70.9984 164.1924 0013863 209.9159 313.7074 14.16565090578192
| Epoch (UTC): | 30 May 2023 12:27:04 |
| Eccentricity: | 0.0013863 |
| inclination: | 70.9984° |
| perigee height: | 827 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 164.1924° |
| argument of perigee: | 209.9159° |
| revolutions per day: | 14.16565090 |
| mean anomaly at epoch: | 313.7074° |
| orbit number at epoch: | 57819 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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