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 23147.09912822 .00000004 00000-0 -95563-5 0 9994
2 28522 82.9445 150.0217 0045371 185.1534 174.9170 13.89718392930479
| Epoch (UTC): | 27 May 2023 02:22:44 |
| Eccentricity: | 0.0045371 |
| inclination: | 82.9445° |
| perigee height: | 896 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 150.0217° |
| argument of perigee: | 185.1534° |
| revolutions per day: | 13.89718392 |
| mean anomaly at epoch: | 174.9170° |
| orbit number at epoch: | 93047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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