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 39222U 13041A 23266.56787604 .00000086 00000-0 00000-0 0 9993
2 39222 0.0122 193.4318 0000141 305.3611 292.6081 1.00272029 36043
| Epoch (UTC): | 23 September 2023 13:37:44 |
| Eccentricity: | 0.0000141 |
| inclination: | 0.0122° |
| perigee height: | 35785 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 193.4318° |
| argument of perigee: | 305.3611° |
| revolutions per day: | 1.00272029 |
| mean anomaly at epoch: | 292.6081° |
| orbit number at epoch: | 3604 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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