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 41747U 26144.95566997 +.00000000 +00000-0 +00000-0 0 00009
2 41747 0.0120 348.4799 0001469 337.3045 329.3146 1.00269212 08
| Epoch (UTC): | 24 May 2026 22:56:09 |
| Eccentricity: | 0.0001469 |
| inclination: | 0.0120° |
| perigee height: | 35781 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 348.4799° |
| argument of perigee: | 337.3045° |
| revolutions per day: | 1.00269212 |
| mean anomaly at epoch: | 329.3146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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