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 33433U 26150.08691300 +.00000000 +00000-0 +87972-4 0 00007
2 33433 98.6072 176.8067 0013551 182.5701 177.5415 14.30795668 03
| Epoch (UTC): | 30 May 2026 02:05:09 |
| Eccentricity: | 0.0013551 |
| inclination: | 98.6072° |
| perigee height: | 779 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 176.8067° |
| argument of perigee: | 182.5701° |
| revolutions per day: | 14.30795668 |
| mean anomaly at epoch: | 177.5415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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