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 11427U 79060B 22227.78812251 .00000095 00000-0 40404-4 0 9996
2 11427 74.0178 153.5132 0020612 204.6760 155.3410 14.37560641258562
| Epoch (UTC): | 15 August 2022 18:54:53 |
| Eccentricity: | 0.0020612 |
| inclination: | 74.0178° |
| perigee height: | 752 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 153.5132° |
| argument of perigee: | 204.6760° |
| revolutions per day: | 14.37560641 |
| mean anomaly at epoch: | 155.3410° |
| orbit number at epoch: | 25856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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