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 22222.48106801 -.00000210 00000-0 -84816-4 0 9997
2 20624 71.0384 238.4895 0013652 30.3508 329.8402 14.14398386662766
| Epoch (UTC): | 10 August 2022 11:32:44 |
| Eccentricity: | 0.0013652 |
| inclination: | 71.0384° |
| perigee height: | 834 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 238.4895° |
| argument of perigee: | 30.3508° |
| revolutions per day: | 14.14398386 |
| mean anomaly at epoch: | 329.8402° |
| orbit number at epoch: | 66276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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