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 00047U 26099.66950097 +.00000000 +00000-0 +22852-3 0 00004
2 00047 66.6645 230.7158 0219896 190.1640 169.4986 14.45247426 00
| Epoch (UTC): | 09 April 2026 16:04:04 |
| Eccentricity: | 0.0219896 |
| inclination: | 66.6645° |
| perigee height: | 585 km |
| apogee height: | 898 km |
| right ascension of ascending node: | 230.7158° |
| argument of perigee: | 190.1640° |
| revolutions per day: | 14.45247426 |
| mean anomaly at epoch: | 169.4986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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