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 32763U 26145.31850281 +.00000000 +00000-0 +00000-0 0 00000
2 32763 5.5332 36.2121 0002179 11.0813 217.4177 1.00269582 01
| Epoch (UTC): | 25 May 2026 07:38:38 |
| Eccentricity: | 0.0002179 |
| inclination: | 5.5332° |
| perigee height: | 35778 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 36.2121° |
| argument of perigee: | 11.0813° |
| revolutions per day: | 1.00269582 |
| mean anomaly at epoch: | 217.4177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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