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 23271.17936852 .00005764 00000-0 29752-3 0 9990
2 20580 28.4695 302.2681 0002573 62.1623 348.0153 15.14182267637344
| Epoch (UTC): | 28 September 2023 04:18:17 |
| Eccentricity: | 0.0002573 |
| inclination: | 28.4695° |
| perigee height: | 521 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 302.2681° |
| argument of perigee: | 62.1623° |
| revolutions per day: | 15.14182267 |
| mean anomaly at epoch: | 348.0153° |
| orbit number at epoch: | 63734 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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