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 26049.73308343 +.00000000 +00000-0 +11193-3 0 00003
2 00046 66.6878 191.1410 0192940 20.3073 340.5575 14.54653917 04
| Epoch (UTC): | 18 February 2026 17:35:38 |
| Eccentricity: | 0.0192940 |
| inclination: | 66.6878° |
| perigee height: | 574 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 191.1410° |
| argument of perigee: | 20.3073° |
| revolutions per day: | 14.54653917 |
| mean anomaly at epoch: | 340.5575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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