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 41745U 26138.46284808 +.00000000 +00000-0 +00000-0 0 00004
2 41745 4.0951 77.6278 0010837 139.4561 308.6113 1.00278714 09
| Epoch (UTC): | 18 May 2026 11:06:30 |
| Eccentricity: | 0.0010837 |
| inclination: | 4.0951° |
| perigee height: | 35739 km |
| apogee height: | 35830 km |
| right ascension of ascending node: | 77.6278° |
| argument of perigee: | 139.4561° |
| revolutions per day: | 1.00278714 |
| mean anomaly at epoch: | 308.6113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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