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 40617U 26152.22448630 +.00000000 +00000-0 +00000-0 0 00006
2 40617 0.0344 68.6877 0003226 358.4482 315.4118 1.00270830 04
| Epoch (UTC): | 01 June 2026 05:23:15 |
| Eccentricity: | 0.0003226 |
| inclination: | 0.0344° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 68.6877° |
| argument of perigee: | 358.4482° |
| revolutions per day: | 1.00270830 |
| mean anomaly at epoch: | 315.4118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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