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 39430U 26101.51593389 +.00000000 +00000-0 +18810-3 0 00006
2 39430 97.6542 306.1715 0127767 291.9815 66.7855 14.69225773 05
| Epoch (UTC): | 11 April 2026 12:22:56 |
| Eccentricity: | 0.0127767 |
| inclination: | 97.6542° |
| perigee height: | 574 km |
| apogee height: | 754 km |
| right ascension of ascending node: | 306.1715° |
| argument of perigee: | 291.9815° |
| revolutions per day: | 14.69225773 |
| mean anomaly at epoch: | 66.7855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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