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 23151.79157020 .00000006 00000-0 27154-4 0 9994
2 22220 70.9984 161.5126 0013808 208.2251 324.1226 14.16565311578372
| Epoch (UTC): | 31 May 2023 18:59:51 |
| Eccentricity: | 0.0013808 |
| inclination: | 70.9984° |
| perigee height: | 827 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 161.5126° |
| argument of perigee: | 208.2251° |
| revolutions per day: | 14.16565311 |
| mean anomaly at epoch: | 324.1226° |
| orbit number at epoch: | 57837 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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