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 39679U 14021B 22140.55089742 .00002885 00000-0 14998-3 0 9998
2 39679 51.6153 85.8848 0164886 221.1487 137.6956 15.08544537444906
| Epoch (UTC): | 20 May 2022 13:13:17 |
| Eccentricity: | 0.0164886 |
| inclination: | 51.6153° |
| perigee height: | 426 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 85.8848° |
| argument of perigee: | 221.1487° |
| revolutions per day: | 15.08544537 |
| mean anomaly at epoch: | 137.6956° |
| orbit number at epoch: | 44490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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