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 22182.57302393 -.00000007 00000-0 29110-4 0 9991
2 26931 67.0519 21.9531 0007418 261.6085 98.4176 14.30712435 83422
| Epoch (UTC): | 01 July 2022 13:45:09 |
| Eccentricity: | 0.0007418 |
| inclination: | 67.0519° |
| perigee height: | 784 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 21.9531° |
| argument of perigee: | 261.6085° |
| revolutions per day: | 14.30712435 |
| mean anomaly at epoch: | 98.4176° |
| orbit number at epoch: | 8342 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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