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 43786U 26111.09352251 +.00000000 +00000-0 +29952-3 0 00009
2 43786 97.4081 163.7611 0012803 184.3156 175.7970 15.18305968 08
| Epoch (UTC): | 21 April 2026 02:14:40 |
| Eccentricity: | 0.0012803 |
| inclination: | 97.4081° |
| perigee height: | 502 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 163.7611° |
| argument of perigee: | 184.3156° |
| revolutions per day: | 15.18305968 |
| mean anomaly at epoch: | 175.7970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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