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 63660U 26144.89049676 +.00000000 +00000-0 +10840-2 0 00005
2 63660 43.0003 294.6167 0001861 267.9850 92.0788 15.27605847 00
| Epoch (UTC): | 24 May 2026 21:22:18 |
| Eccentricity: | 0.0001861 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 294.6167° |
| argument of perigee: | 267.9850° |
| revolutions per day: | 15.27605847 |
| mean anomaly at epoch: | 92.0788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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