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 14781U 26066.79391382 +.00000000 +00000-0 +28120-3 0 00002
2 14781 97.7951 33.5882 0008269 148.9328 211.2380 14.90499739 02
| Epoch (UTC): | 07 March 2026 19:03:14 |
| Eccentricity: | 0.0008269 |
| inclination: | 97.7951° |
| perigee height: | 591 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 33.5882° |
| argument of perigee: | 148.9328° |
| revolutions per day: | 14.90499739 |
| mean anomaly at epoch: | 211.2380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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