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 22826U 93061D 25197.77852524 .00000067 00000-0 42315-4 0 9995
2 22826 98.7294 259.4024 0008695 355.8107 4.3001 14.31223409659337
| Epoch (UTC): | 16 July 2025 18:41:04 |
| Eccentricity: | 0.0008695 |
| inclination: | 98.7294° |
| perigee height: | 781 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 259.4024° |
| argument of perigee: | 355.8107° |
| revolutions per day: | 14.31223409 |
| mean anomaly at epoch: | 4.3001° |
| orbit number at epoch: | 65933 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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