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 65333U 26145.45575005 +.00000000 +00000-0 +43735-3 0 00007
2 65333 53.1596 209.9094 0000996 83.1961 276.9154 15.31713781 07
| Epoch (UTC): | 25 May 2026 10:56:16 |
| Eccentricity: | 0.0000996 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 209.9094° |
| argument of perigee: | 83.1961° |
| revolutions per day: | 15.31713781 |
| mean anomaly at epoch: | 276.9154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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