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 22224.78752711 .00000218 00000-0 13764-3 0 9999
2 20625 70.9990 157.6745 0012822 133.3261 226.8933 14.14696365663823
| Epoch (UTC): | 12 August 2022 18:54:02 |
| Eccentricity: | 0.0012822 |
| inclination: | 70.9990° |
| perigee height: | 834 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 157.6745° |
| argument of perigee: | 133.3261° |
| revolutions per day: | 14.14696365 |
| mean anomaly at epoch: | 226.8933° |
| orbit number at epoch: | 66382 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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