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 is defined by the following mean orbital elements,
1 32791U 26073.43612563 +.00000000 +00000-0 +80965-3 0 00004
2 32791 97.7516 67.0643 0000660 332.7648 27.3557 15.29309746 05
| Epoch (UTC): | 14 March 2026 10:28:01 |
| Eccentricity: | 0.0000660 |
| inclination: | 97.7516° |
| perigee height: | 477 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 67.0643° |
| argument of perigee: | 332.7648° |
| revolutions per day: | 15.29309746 |
| mean anomaly at epoch: | 27.3557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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