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 22141.28783368 .00004380 00000-0 24853-3 0 9999
2 20580 28.4712 348.7951 0002853 100.0255 64.2395 15.10474764562101
| Epoch (UTC): | 21 May 2022 06:54:28 |
| Eccentricity: | 0.0002853 |
| inclination: | 28.4712° |
| perigee height: | 533 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 348.7951° |
| argument of perigee: | 100.0255° |
| revolutions per day: | 15.10474764 |
| mean anomaly at epoch: | 64.2395° |
| orbit number at epoch: | 56210 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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