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 26042.10131919 +.00000000 +00000-0 +13578-3 0 00009
2 00046 66.6866 211.9384 0192234 26.1315 334.9342 14.54643186 07
| Epoch (UTC): | 11 February 2026 02:25:53 |
| Eccentricity: | 0.0192234 |
| inclination: | 66.6866° |
| perigee height: | 574 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 211.9384° |
| argument of perigee: | 26.1315° |
| revolutions per day: | 14.54643186 |
| mean anomaly at epoch: | 334.9342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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