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 26040.86373013 +.00000000 +00000-0 +14599-3 0 00007
2 00046 66.6864 215.3111 0192126 27.0808 334.0167 14.54641302 02
| Epoch (UTC): | 09 February 2026 20:43:46 |
| Eccentricity: | 0.0192126 |
| inclination: | 66.6864° |
| perigee height: | 574 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 215.3111° |
| argument of perigee: | 27.0808° |
| revolutions per day: | 14.54641302 |
| mean anomaly at epoch: | 334.0167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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