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 53600U 26145.36051398 +.00000000 +00000-0 -22901-4 0 00009
2 53600 53.2146 260.3333 0001242 88.6508 271.4627 15.08840142 03
| Epoch (UTC): | 25 May 2026 08:39:08 |
| Eccentricity: | 0.0001242 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 260.3333° |
| argument of perigee: | 88.6508° |
| revolutions per day: | 15.08840142 |
| mean anomaly at epoch: | 271.4627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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