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 23030.56903539 .00003617 00000-0 19590-3 0 9996
2 20580 28.4703 102.7539 0002087 340.2053 126.1085 15.11796735600602
| Epoch (UTC): | 30 January 2023 13:39:24 |
| Eccentricity: | 0.0002087 |
| inclination: | 28.4703° |
| perigee height: | 529 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 102.7539° |
| argument of perigee: | 340.2053° |
| revolutions per day: | 15.11796735 |
| mean anomaly at epoch: | 126.1085° |
| orbit number at epoch: | 60060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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