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 42759U 17034B 22139.71931874 .00004006 00000-0 24405-3 0 9997
2 42759 43.0161 131.0578 0007373 106.8178 62.2849 15.11677581272004
| Epoch (UTC): | 19 May 2022 17:15:49 |
| Eccentricity: | 0.0007373 |
| inclination: | 43.0161° |
| perigee height: | 526 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 131.0578° |
| argument of perigee: | 106.8178° |
| revolutions per day: | 15.11677581 |
| mean anomaly at epoch: | 62.2849° |
| orbit number at epoch: | 27200 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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