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 22676U 93036B 23151.45574986 .00000328 00000-0 12577-3 0 9992
2 22676 74.0403 164.7235 0018375 15.6786 344.4931 14.34304231566705
| Epoch (UTC): | 31 May 2023 10:56:16 |
| Eccentricity: | 0.0018375 |
| inclination: | 74.0403° |
| perigee height: | 764 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 164.7235° |
| argument of perigee: | 15.6786° |
| revolutions per day: | 14.34304231 |
| mean anomaly at epoch: | 344.4931° |
| orbit number at epoch: | 56670 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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