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 22184.90913241 .00001517 00000-0 99670-4 0 9997
2 42759 43.0173 241.9937 0008680 23.1427 145.7855 15.12008027278843
| Epoch (UTC): | 03 July 2022 21:49:09 |
| Eccentricity: | 0.0008680 |
| inclination: | 43.0173° |
| perigee height: | 524 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 241.9937° |
| argument of perigee: | 23.1427° |
| revolutions per day: | 15.12008027 |
| mean anomaly at epoch: | 145.7855° |
| orbit number at epoch: | 27884 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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