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 26150.50529315 +.00000000 +00000-0 +68228-3 0 00008
2 32791 97.7511 147.5679 0003551 49.7745 310.3805 15.32079827 07
| Epoch (UTC): | 30 May 2026 12:07:37 |
| Eccentricity: | 0.0003551 |
| inclination: | 97.7511° |
| perigee height: | 467 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 147.5679° |
| argument of perigee: | 49.7745° |
| revolutions per day: | 15.32079827 |
| mean anomaly at epoch: | 310.3805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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