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 41530U 00055NE 22265.57847519 .00004337 00000-0 13894-2 0 9990
2 41530 98.7839 35.6629 0087746 37.6509 323.0775 14.37868140335653
| Epoch (UTC): | 22 September 2022 13:53:00 |
| Eccentricity: | 0.0087746 |
| inclination: | 98.7839° |
| perigee height: | 703 km |
| apogee height: | 828 km |
| right ascension of ascending node: | 35.6629° |
| argument of perigee: | 37.6509° |
| revolutions per day: | 14.37868140 |
| mean anomaly at epoch: | 323.0775° |
| orbit number at epoch: | 33565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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