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 23153.50700145 -.00000008 00000-0 -19182-4 0 9997
2 28522 82.9446 145.1581 0045865 166.8532 193.3840 13.89717961931360
| Epoch (UTC): | 02 June 2023 12:10:04 |
| Eccentricity: | 0.0045865 |
| inclination: | 82.9446° |
| perigee height: | 896 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 145.1581° |
| argument of perigee: | 166.8532° |
| revolutions per day: | 13.89717961 |
| mean anomaly at epoch: | 193.3840° |
| orbit number at epoch: | 93136 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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