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 00046U 26037.83850512 +.00000000 +00000-0 +18549-3 0 00003
2 00046 66.6863 223.5559 0191856 29.3964 331.7774 14.54636577 01
| Epoch (UTC): | 06 February 2026 20:07:26 |
| Eccentricity: | 0.0191856 |
| inclination: | 66.6863° |
| perigee height: | 575 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 223.5559° |
| argument of perigee: | 29.3964° |
| revolutions per day: | 14.54636577 |
| mean anomaly at epoch: | 331.7774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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