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 41922U 17003F 23151.54131963 .00000278 00000-0 92116-4 0 9993
2 41922 86.4010 193.3924 0002455 90.5879 269.5598 14.34220332333797
| Epoch (UTC): | 31 May 2023 12:59:30 |
| Eccentricity: | 0.0002455 |
| inclination: | 86.4010° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 193.3924° |
| argument of perigee: | 90.5879° |
| revolutions per day: | 14.34220332 |
| mean anomaly at epoch: | 269.5598° |
| orbit number at epoch: | 33379 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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