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 23150.48306112 -.00000009 00000-0 -20499-4 0 9991
2 28522 82.9445 147.4532 0045638 175.4690 184.6897 13.89718132930881
| Epoch (UTC): | 30 May 2023 11:35:36 |
| Eccentricity: | 0.0045638 |
| inclination: | 82.9445° |
| perigee height: | 896 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 147.4532° |
| argument of perigee: | 175.4690° |
| revolutions per day: | 13.89718132 |
| mean anomaly at epoch: | 184.6897° |
| orbit number at epoch: | 93088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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