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 65529U 26145.14837943 +.00000000 +00000-0 +22814-3 0 00007
2 65529 97.4498 214.7644 0001841 142.6325 217.5030 15.05647856 00
| Epoch (UTC): | 25 May 2026 03:33:39 |
| Eccentricity: | 0.0001841 |
| inclination: | 97.4498° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.7644° |
| argument of perigee: | 142.6325° |
| revolutions per day: | 15.05647856 |
| mean anomaly at epoch: | 217.5030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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