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 26145.47583941 +.00000000 +00000-0 +56920-3 0 00009
2 32791 97.7521 142.3050 0004202 58.8151 301.3501 15.31851938 03
| Epoch (UTC): | 25 May 2026 11:25:12 |
| Eccentricity: | 0.0004202 |
| inclination: | 97.7521° |
| perigee height: | 467 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 142.3050° |
| argument of perigee: | 58.8151° |
| revolutions per day: | 15.31851938 |
| mean anomaly at epoch: | 301.3501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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