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 26066.98587382 +.00000000 +00000-0 +42489-3 0 00002
2 39430 97.6567 273.7975 0130354 42.9558 318.1738 14.69091129 03
| Epoch (UTC): | 07 March 2026 23:39:39 |
| Eccentricity: | 0.0130354 |
| inclination: | 97.6567° |
| perigee height: | 572 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 273.7975° |
| argument of perigee: | 42.9558° |
| revolutions per day: | 14.69091129 |
| mean anomaly at epoch: | 318.1738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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