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 33320U 26145.64507469 +.00000000 +00000-0 +11031-3 0 00002
2 33320 97.6677 132.3577 0018035 208.6454 151.3772 14.83925504 06
| Epoch (UTC): | 25 May 2026 15:28:54 |
| Eccentricity: | 0.0018035 |
| inclination: | 97.6677° |
| perigee height: | 604 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 132.3577° |
| argument of perigee: | 208.6454° |
| revolutions per day: | 14.83925504 |
| mean anomaly at epoch: | 151.3772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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