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 data is extracted from the following two-line orbital elements,
1 26069U 00006A 25343.14357822 .00000193 00000-0 12700-3 0 9994
2 26069 70.9947 349.8665 0012824 224.7295 135.2794 14.13851909597092
| Epoch (UTC): | 09 December 2025 03:26:45 |
| Eccentricity: | 0.0012824 |
| inclination: | 70.9947° |
| perigee height: | 837 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 349.8665° |
| argument of perigee: | 224.7295° |
| revolutions per day: | 14.13851909 |
| mean anomaly at epoch: | 135.2794° |
| orbit number at epoch: | 59709 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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