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 42778U 17036P 22176.64543869 .00006165 00000-0 23414-3 0 9993
2 42778 97.2047 217.4651 0008821 301.3785 58.6591 15.27131675278156
| Epoch (UTC): | 25 June 2022 15:29:25 |
| Eccentricity: | 0.0008821 |
| inclination: | 97.2047° |
| perigee height: | 478 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 217.4651° |
| argument of perigee: | 301.3785° |
| revolutions per day: | 15.27131675 |
| mean anomaly at epoch: | 58.6591° |
| orbit number at epoch: | 27815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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