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 43776U 26145.08850644 +.00000000 +00000-0 +93781-4 0 00005
2 43776 97.4395 186.3131 0021791 80.6071 279.7619 15.05539548 07
| Epoch (UTC): | 25 May 2026 02:07:26 |
| Eccentricity: | 0.0021791 |
| inclination: | 97.4395° |
| perigee height: | 535 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 186.3131° |
| argument of perigee: | 80.6071° |
| revolutions per day: | 15.05539548 |
| mean anomaly at epoch: | 279.7619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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