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 42017U 17008BX 22177.69225762 .00014155 00000-0 41996-3 0 9996
2 42017 97.2689 243.6728 0004925 190.8255 169.2883 15.34909548298496
| Epoch (UTC): | 26 June 2022 16:36:51 |
| Eccentricity: | 0.0004925 |
| inclination: | 97.2689° |
| perigee height: | 458 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 243.6728° |
| argument of perigee: | 190.8255° |
| revolutions per day: | 15.34909548 |
| mean anomaly at epoch: | 169.2883° |
| orbit number at epoch: | 29849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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