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 22175.85914209 .00006130 00000-0 23290-3 0 9999
2 42778 97.2048 216.7057 0008863 304.7513 55.2891 15.27120865278033
| Epoch (UTC): | 24 June 2022 20:37:09 |
| Eccentricity: | 0.0008863 |
| inclination: | 97.2048° |
| perigee height: | 478 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 216.7057° |
| argument of perigee: | 304.7513° |
| revolutions per day: | 15.27120865 |
| mean anomaly at epoch: | 55.2891° |
| orbit number at epoch: | 27803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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