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 23152.11486387 .00000154 00000-0 96166-4 0 9994
2 19120 71.0159 49.1255 0019727 93.5844 266.7538 14.19316629814690
| Epoch (UTC): | 01 June 2023 02:45:24 |
| Eccentricity: | 0.0019727 |
| inclination: | 71.0159° |
| perigee height: | 813 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 49.1255° |
| argument of perigee: | 93.5844° |
| revolutions per day: | 14.19316629 |
| mean anomaly at epoch: | 266.7538° |
| orbit number at epoch: | 81469 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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