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 20847U 90081K 22147.81447018 .00018664 00000-0 18608-2 0 9998
2 20847 98.5543 184.1126 0014427 38.8385 321.3865 14.91548430673411
| Epoch (UTC): | 27 May 2022 19:32:50 |
| Eccentricity: | 0.0014427 |
| inclination: | 98.5543° |
| perigee height: | 583 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 184.1126° |
| argument of perigee: | 38.8385° |
| revolutions per day: | 14.91548430 |
| mean anomaly at epoch: | 321.3865° |
| orbit number at epoch: | 67341 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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