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 19120U 88039B 23157.04829153 .00000079 00000-0 60478-4 0 9996
2 19120 71.0158 38.6992 0019751 85.1515 275.1865 14.19318404815667
| Epoch (UTC): | 06 June 2023 01:09:32 |
| Eccentricity: | 0.0019751 |
| inclination: | 71.0158° |
| perigee height: | 813 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 38.6992° |
| argument of perigee: | 85.1515° |
| revolutions per day: | 14.19318404 |
| mean anomaly at epoch: | 275.1865° |
| orbit number at epoch: | 81566 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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