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 26045.88283132 +.00000000 +00000-0 +11048-3 0 00002
2 00046 66.6872 201.6333 0192583 23.2432 337.7241 14.54648337 01
| Epoch (UTC): | 14 February 2026 21:11:16 |
| Eccentricity: | 0.0192583 |
| inclination: | 66.6872° |
| perigee height: | 574 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 201.6333° |
| argument of perigee: | 23.2432° |
| revolutions per day: | 14.54648337 |
| mean anomaly at epoch: | 337.7241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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