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 23159.58547946 -.00000066 00000-0 -87708-5 0 9998
2 19120 71.0158 33.3370 0019750 80.8345 279.5013 14.19318899816023
| Epoch (UTC): | 08 June 2023 14:03:05 |
| Eccentricity: | 0.0019750 |
| inclination: | 71.0158° |
| perigee height: | 813 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 33.3370° |
| argument of perigee: | 80.8345° |
| revolutions per day: | 14.19318899 |
| mean anomaly at epoch: | 279.5013° |
| orbit number at epoch: | 81602 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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