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 26931U 01043C 22139.72040220 .00000245 00000-0 12523-3 0 9990
2 26931 67.0493 132.5616 0007940 267.6529 92.3663 14.30698136 77456
| Epoch (UTC): | 19 May 2022 17:17:22 |
| Eccentricity: | 0.0007940 |
| inclination: | 67.0493° |
| perigee height: | 784 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 132.5616° |
| argument of perigee: | 267.6529° |
| revolutions per day: | 14.30698136 |
| mean anomaly at epoch: | 92.3663° |
| orbit number at epoch: | 7745 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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