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 11783U 26146.37002454 +.00000000 +00000-0 +00000-0 0 00007
2 11783 61.8484 249.1725 0552174 51.7339 322.7442 2.03455927 06
| Epoch (UTC): | 26 May 2026 08:52:50 |
| Eccentricity: | 0.0552174 |
| inclination: | 61.8484° |
| perigee height: | 18477 km |
| apogee height: | 21383 km |
| right ascension of ascending node: | 249.1725° |
| argument of perigee: | 51.7339° |
| revolutions per day: | 2.03455927 |
| mean anomaly at epoch: | 322.7442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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