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 20580U 90037B 23081.79479084 .00005842 00000-0 31702-3 0 9991
2 20580 28.4692 122.5230 0002923 161.2445 349.4656 15.12439732608639
| Epoch (UTC): | 22 March 2023 19:04:29 |
| Eccentricity: | 0.0002923 |
| inclination: | 28.4692° |
| perigee height: | 527 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 122.5230° |
| argument of perigee: | 161.2445° |
| revolutions per day: | 15.12439732 |
| mean anomaly at epoch: | 349.4656° |
| orbit number at epoch: | 60863 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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