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 23151.20694382 .00000039 00000-0 43682-4 0 9997
2 22220 70.9984 162.7435 0013834 208.9992 222.8571 14.16565246578628
| Epoch (UTC): | 31 May 2023 04:57:59 |
| Eccentricity: | 0.0013834 |
| inclination: | 70.9984° |
| perigee height: | 827 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 162.7435° |
| argument of perigee: | 208.9992° |
| revolutions per day: | 14.16565246 |
| mean anomaly at epoch: | 222.8571° |
| orbit number at epoch: | 57862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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