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 26131.82057969 +.00000000 +00000-0 +60024-4 0 00008
2 00046 66.6884 327.3930 0199921 319.0463 39.5773 14.54835441 07
| Epoch (UTC): | 11 May 2026 19:41:38 |
| Eccentricity: | 0.0199921 |
| inclination: | 66.6884° |
| perigee height: | 568 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 327.3930° |
| argument of perigee: | 319.0463° |
| revolutions per day: | 14.54835441 |
| mean anomaly at epoch: | 39.5773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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