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 63511U 26145.27132785 +.00000000 +00000-0 +48974-3 0 00007
2 63511 53.1589 144.2602 0000928 82.5202 277.5905 15.31722922 05
| Epoch (UTC): | 25 May 2026 06:30:42 |
| Eccentricity: | 0.0000928 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 144.2602° |
| argument of perigee: | 82.5202° |
| revolutions per day: | 15.31722922 |
| mean anomaly at epoch: | 277.5905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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