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 26155.31605132 +.00000000 +00000-0 +33944-3 0 00008
2 39430 97.6486 356.5910 0129981 118.4120 243.0259 14.69407998 09
| Epoch (UTC): | 04 June 2026 07:35:06 |
| Eccentricity: | 0.0129981 |
| inclination: | 97.6486° |
| perigee height: | 571 km |
| apogee height: | 754 km |
| right ascension of ascending node: | 356.5910° |
| argument of perigee: | 118.4120° |
| revolutions per day: | 14.69407998 |
| mean anomaly at epoch: | 243.0259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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