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 19649U 88102A 22227.81059917 .00000301 00000-0 18066-3 0 9991
2 19649 70.9997 67.9142 0006654 313.5201 46.5368 14.14770073741252
| Epoch (UTC): | 15 August 2022 19:27:15 |
| Eccentricity: | 0.0006654 |
| inclination: | 70.9997° |
| perigee height: | 838 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 67.9142° |
| argument of perigee: | 313.5201° |
| revolutions per day: | 14.14770073 |
| mean anomaly at epoch: | 46.5368° |
| orbit number at epoch: | 74125 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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