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 22148.53630990 .00002720 00000-0 15009-3 0 9995
2 20580 28.4703 300.7717 0002524 173.5140 244.6953 15.10519890563208
| Epoch (UTC): | 28 May 2022 12:52:17 |
| Eccentricity: | 0.0002524 |
| inclination: | 28.4703° |
| perigee height: | 533 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 300.7717° |
| argument of perigee: | 173.5140° |
| revolutions per day: | 15.10519890 |
| mean anomaly at epoch: | 244.6953° |
| orbit number at epoch: | 56320 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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