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 23151.82039317 .00000277 00000-0 91941-4 0 9998
2 41922 86.4009 193.2760 0002457 90.4712 269.6765 14.34220464333837
| Epoch (UTC): | 31 May 2023 19:41:21 |
| Eccentricity: | 0.0002457 |
| inclination: | 86.4009° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 193.2760° |
| argument of perigee: | 90.4712° |
| revolutions per day: | 14.34220464 |
| mean anomaly at epoch: | 269.6765° |
| orbit number at epoch: | 33383 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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