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 22180.90445424 .00003935 00000-0 15024-3 0 9995
2 42778 97.2035 221.5783 0008695 282.7890 77.2378 15.27180620278809
| Epoch (UTC): | 29 June 2022 21:42:24 |
| Eccentricity: | 0.0008695 |
| inclination: | 97.2035° |
| perigee height: | 478 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 221.5783° |
| argument of perigee: | 282.7890° |
| revolutions per day: | 15.27180620 |
| mean anomaly at epoch: | 77.2378° |
| orbit number at epoch: | 27880 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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