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 26040.58871016 +.00000000 +00000-0 +15132-3 0 00006
2 00046 66.6864 216.0606 0192100 27.2916 333.8129 14.54640951 07
| Epoch (UTC): | 09 February 2026 14:07:44 |
| Eccentricity: | 0.0192100 |
| inclination: | 66.6864° |
| perigee height: | 574 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 216.0606° |
| argument of perigee: | 27.2916° |
| revolutions per day: | 14.54640951 |
| mean anomaly at epoch: | 333.8129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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