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 26048.83927603 +.00000000 +00000-0 +10777-3 0 00006
2 00046 66.6875 193.5766 0192862 20.9884 339.9005 14.54652599 05
| Epoch (UTC): | 17 February 2026 20:08:33 |
| Eccentricity: | 0.0192862 |
| inclination: | 66.6875° |
| perigee height: | 574 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 193.5766° |
| argument of perigee: | 20.9884° |
| revolutions per day: | 14.54652599 |
| mean anomaly at epoch: | 339.9005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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