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 26038.21529727 +.00000000 +00000-0 +10148-2 0 00005
2 32791 97.7495 30.4199 0005326 67.8376 292.3427 15.27724830 02
| Epoch (UTC): | 07 February 2026 05:10:01 |
| Eccentricity: | 0.0005326 |
| inclination: | 97.7495° |
| perigee height: | 479 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 30.4199° |
| argument of perigee: | 67.8376° |
| revolutions per day: | 15.27724830 |
| mean anomaly at epoch: | 292.3427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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