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 23152.16923511 .00000280 00000-0 92901-4 0 9995
2 41922 86.4009 193.1304 0002462 90.3751 269.7727 14.34220660333880
| Epoch (UTC): | 01 June 2023 04:03:41 |
| Eccentricity: | 0.0002462 |
| inclination: | 86.4009° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 193.1304° |
| argument of perigee: | 90.3751° |
| revolutions per day: | 14.34220660 |
| mean anomaly at epoch: | 269.7727° |
| orbit number at epoch: | 33388 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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