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 22181.93643256 .00002471 00000-0 15413-3 0 9995
2 42759 43.0172 258.3783 0009574 5.4536 163.7191 15.12002225278397
| Epoch (UTC): | 30 June 2022 22:28:27 |
| Eccentricity: | 0.0009574 |
| inclination: | 43.0172° |
| perigee height: | 523 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 258.3783° |
| argument of perigee: | 5.4536° |
| revolutions per day: | 15.12002225 |
| mean anomaly at epoch: | 163.7191° |
| orbit number at epoch: | 27839 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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