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 21102.74761468 .00000163 00000-0 10958-3 0 9999
2 20625 70.9964 99.9850 0013429 155.4675 204.7089 14.14663473595192
| Epoch (UTC): | 12 April 2021 17:56:33 |
| Eccentricity: | 0.0013429 |
| inclination: | 70.9964° |
| perigee height: | 834 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 99.9850° |
| argument of perigee: | 155.4675° |
| revolutions per day: | 14.14663473 |
| mean anomaly at epoch: | 204.7089° |
| orbit number at epoch: | 59519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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