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 26039.19559714 +.00000000 +00000-0 +32711-3 0 00000
2 39430 97.6578 247.7380 0130551 131.3120 229.9411 14.68968734 04
| Epoch (UTC): | 08 February 2026 04:41:39 |
| Eccentricity: | 0.0130551 |
| inclination: | 97.6578° |
| perigee height: | 572 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 247.7380° |
| argument of perigee: | 131.3120° |
| revolutions per day: | 14.68968734 |
| mean anomaly at epoch: | 229.9411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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