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 20625U 90046B 21018.88646034 .00000292 00000-0 17630-3 0 9998
2 20625 70.9991 276.0101 0016428 273.7424 86.1820 14.14662561583084
| Epoch (UTC): | 18 January 2021 21:16:30 |
| Eccentricity: | 0.0016428 |
| inclination: | 70.9991° |
| perigee height: | 831 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 276.0101° |
| argument of perigee: | 273.7424° |
| revolutions per day: | 14.14662561 |
| mean anomaly at epoch: | 86.1820° |
| orbit number at epoch: | 58308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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