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 41667U 26066.50843466 +.00000000 +00000-0 +88788-3 0 00005
2 41667 98.7678 171.8069 0030378 110.8885 249.5551 14.25441907 03
| Epoch (UTC): | 07 March 2026 12:12:08 |
| Eccentricity: | 0.0030378 |
| inclination: | 98.7678° |
| perigee height: | 785 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 171.8069° |
| argument of perigee: | 110.8885° |
| revolutions per day: | 14.25441907 |
| mean anomaly at epoch: | 249.5551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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