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 63320U 26144.88624153 +.00000000 +00000-0 +41105-3 0 00005
2 63320 43.0010 309.8987 0001361 272.0891 87.9805 15.27595308 00
| Epoch (UTC): | 24 May 2026 21:16:11 |
| Eccentricity: | 0.0001361 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.8987° |
| argument of perigee: | 272.0891° |
| revolutions per day: | 15.27595308 |
| mean anomaly at epoch: | 87.9805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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