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 42689U 17022A 22193.82779864 0.00018000 00000-0 16528-3 0 06
2 42689 49.9967 119.2555 0002172 113.0682 246.9316 15.66976839 07
| Epoch (UTC): | 12 July 2022 19:52:01 |
| Eccentricity: | 0.0002172 |
| inclination: | 49.9967° |
| perigee height: | 366 km |
| apogee height: | 369 km |
| right ascension of ascending node: | 119.2555° |
| argument of perigee: | 113.0682° |
| revolutions per day: | 15.66976839 |
| mean anomaly at epoch: | 246.9316° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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