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 26108.22872765 +.00000000 +00000-0 +41088-3 0 00005
2 32791 97.7527 103.3650 0004417 130.7985 229.3639 15.30679504 02
| Epoch (UTC): | 18 April 2026 05:29:22 |
| Eccentricity: | 0.0004417 |
| inclination: | 97.7527° |
| perigee height: | 471 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 103.3650° |
| argument of perigee: | 130.7985° |
| revolutions per day: | 15.30679504 |
| mean anomaly at epoch: | 229.3639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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