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 20624U 90046A 21018.64729543 .00000035 00000-0 42856-4 0 9992
2 20624 71.0422 349.3914 0015424 196.4043 163.6582 14.14354356582617
| Epoch (UTC): | 18 January 2021 15:32:06 |
| Eccentricity: | 0.0015424 |
| inclination: | 71.0422° |
| perigee height: | 833 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 349.3914° |
| argument of perigee: | 196.4043° |
| revolutions per day: | 14.14354356 |
| mean anomaly at epoch: | 163.6582° |
| orbit number at epoch: | 58261 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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