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 39429U 26111.89598795 +.00000000 +00000-0 +26720-3 0 00001
2 39429 97.6698 334.6146 0113501 206.7541 152.7787 14.75937554 04
| Epoch (UTC): | 21 April 2026 21:30:13 |
| Eccentricity: | 0.0113501 |
| inclination: | 97.6698° |
| perigee height: | 562 km |
| apogee height: | 722 km |
| right ascension of ascending node: | 334.6146° |
| argument of perigee: | 206.7541° |
| revolutions per day: | 14.75937554 |
| mean anomaly at epoch: | 152.7787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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