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 23156.14970891 -.00000213 00000-0 -82492-4 0 9995
2 22220 70.9984 152.3370 0013563 202.1578 228.4732 14.16564820579322
| Epoch (UTC): | 05 June 2023 03:35:34 |
| Eccentricity: | 0.0013563 |
| inclination: | 70.9984° |
| perigee height: | 827 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 152.3370° |
| argument of perigee: | 202.1578° |
| revolutions per day: | 14.16564820 |
| mean anomaly at epoch: | 228.4732° |
| orbit number at epoch: | 57932 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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