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 26087.50130162 +.00000000 +00000-0 +78688-3 0 00006
2 32791 97.7522 81.7278 0001837 175.4551 184.6705 15.29863940 04
| Epoch (UTC): | 28 March 2026 12:01:52 |
| Eccentricity: | 0.0001837 |
| inclination: | 97.7522° |
| perigee height: | 475 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 81.7278° |
| argument of perigee: | 175.4551° |
| revolutions per day: | 15.29863940 |
| mean anomaly at epoch: | 184.6705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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