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 63658U 26144.72518098 +.00000000 +00000-0 +45961-3 0 00006
2 63658 42.9977 295.9539 0001227 276.5665 83.5046 15.27583930 08
| Epoch (UTC): | 24 May 2026 17:24:15 |
| Eccentricity: | 0.0001227 |
| inclination: | 42.9977° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.9539° |
| argument of perigee: | 276.5665° |
| revolutions per day: | 15.27583930 |
| mean anomaly at epoch: | 83.5046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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