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 65511U 26145.35099957 +.00000000 +00000-0 +72964-3 0 00007
2 65511 53.1583 273.7511 0001605 79.5650 280.5533 15.34411200 02
| Epoch (UTC): | 25 May 2026 08:25:26 |
| Eccentricity: | 0.0001605 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 273.7511° |
| argument of perigee: | 79.5650° |
| revolutions per day: | 15.34411200 |
| mean anomaly at epoch: | 280.5533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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