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 27601U 02056E 22222.51271897 .00000178 00000-0 78517-4 0 9997
2 27601 98.1778 226.0855 0073332 99.8754 61.7724 14.32091896 26891
| Epoch (UTC): | 10 August 2022 12:18:18 |
| Eccentricity: | 0.0073332 |
| inclination: | 98.1778° |
| perigee height: | 732 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 226.0855° |
| argument of perigee: | 99.8754° |
| revolutions per day: | 14.32091896 |
| mean anomaly at epoch: | 61.7724° |
| orbit number at epoch: | 2689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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