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 28522U 05002B 23151.49104121 -.00000014 00000-0 -24050-4 0 9992
2 28522 82.9445 146.6882 0045679 172.6219 187.5628 13.89718029931027
| Epoch (UTC): | 31 May 2023 11:47:05 |
| Eccentricity: | 0.0045679 |
| inclination: | 82.9445° |
| perigee height: | 896 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 146.6882° |
| argument of perigee: | 172.6219° |
| revolutions per day: | 13.89718029 |
| mean anomaly at epoch: | 187.5628° |
| orbit number at epoch: | 93102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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