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 23150.12306821 -.00000007 00000-0 -18836-4 0 9999
2 28522 82.9445 147.7265 0045609 176.4960 183.6533 13.89718171930896
| Epoch (UTC): | 30 May 2023 02:57:13 |
| Eccentricity: | 0.0045609 |
| inclination: | 82.9445° |
| perigee height: | 896 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 147.7265° |
| argument of perigee: | 176.4960° |
| revolutions per day: | 13.89718171 |
| mean anomaly at epoch: | 183.6533° |
| orbit number at epoch: | 93089 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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