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 22177.89039609 .00006807 00000-0 25810-3 0 9998
2 42778 97.2042 218.6673 0008756 295.9898 64.0439 15.27150489278345
| Epoch (UTC): | 26 June 2022 21:22:10 |
| Eccentricity: | 0.0008756 |
| inclination: | 97.2042° |
| perigee height: | 478 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 218.6673° |
| argument of perigee: | 295.9898° |
| revolutions per day: | 15.27150489 |
| mean anomaly at epoch: | 64.0439° |
| orbit number at epoch: | 27834 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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