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 33063U 26088.23438074 +.00000000 +00000-0 +28270-3 0 00005
2 33063 48.4401 79.0889 0005852 145.0227 215.1073 14.80893167 06
| Epoch (UTC): | 29 March 2026 05:37:30 |
| Eccentricity: | 0.0005852 |
| inclination: | 48.4401° |
| perigee height: | 622 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 79.0889° |
| argument of perigee: | 145.0227° |
| revolutions per day: | 14.80893167 |
| mean anomaly at epoch: | 215.1073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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