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 19341.67958177 .00000144 00000-0 99495-4 0 9991
2 20625 70.9999 52.8248 0014408 183.6829 176.4190 14.14645609525609
| Epoch (UTC): | 07 December 2019 16:18:35 |
| Eccentricity: | 0.0014408 |
| inclination: | 70.9999° |
| perigee height: | 833 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 52.8248° |
| argument of perigee: | 183.6829° |
| revolutions per day: | 14.14645609 |
| mean anomaly at epoch: | 176.4190° |
| orbit number at epoch: | 52560 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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