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 24259.78117643 .00000672 00000-0 23279-3 0 9999
2 41922 86.4028 355.6526 0002242 82.1521 277.9930 14.34222998401623
| Epoch (UTC): | 15 September 2024 18:44:53 |
| Eccentricity: | 0.0002242 |
| inclination: | 86.4028° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 355.6526° |
| argument of perigee: | 82.1521° |
| revolutions per day: | 14.34222998 |
| mean anomaly at epoch: | 277.9930° |
| orbit number at epoch: | 40162 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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