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 62659U 26144.80244198 +.00000000 +00000-0 +10411-2 0 00003
2 62659 97.3951 226.2415 0003492 66.6869 293.4737 15.28454415 09
| Epoch (UTC): | 24 May 2026 19:15:30 |
| Eccentricity: | 0.0003492 |
| inclination: | 97.3951° |
| perigee height: | 478 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 226.2415° |
| argument of perigee: | 66.6869° |
| revolutions per day: | 15.28454415 |
| mean anomaly at epoch: | 293.4737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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