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 14659U 26150.42052976 +.00000000 +00000-0 +00000-0 0 00007
2 14659 11.0835 324.7804 0013595 217.1911 160.7993 0.99051209 08
| Epoch (UTC): | 30 May 2026 10:05:33 |
| Eccentricity: | 0.0013595 |
| inclination: | 11.0835° |
| perigee height: | 36074 km |
| apogee height: | 36190 km |
| right ascension of ascending node: | 324.7804° |
| argument of perigee: | 217.1911° |
| revolutions per day: | 0.99051209 |
| mean anomaly at epoch: | 160.7993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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