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 25083.38348224 .00000724 00000-0 30239-3 0 9994
2 26931 67.0521 327.4268 0005610 267.8722 92.1738 14.31670354226219
| Epoch (UTC): | 24 March 2025 09:12:12 |
| Eccentricity: | 0.0005610 |
| inclination: | 67.0521° |
| perigee height: | 782 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 327.4268° |
| argument of perigee: | 267.8722° |
| revolutions per day: | 14.31670354 |
| mean anomaly at epoch: | 92.1738° |
| orbit number at epoch: | 22621 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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