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 22144.91736458 .00005601 00000-0 33534-3 0 9991
2 42759 43.0170 102.4164 0007731 148.3895 262.0624 15.11741540272796
| Epoch (UTC): | 24 May 2022 22:01:00 |
| Eccentricity: | 0.0007731 |
| inclination: | 43.0170° |
| perigee height: | 525 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 102.4164° |
| argument of perigee: | 148.3895° |
| revolutions per day: | 15.11741540 |
| mean anomaly at epoch: | 262.0624° |
| orbit number at epoch: | 27279 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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