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 04327U 26032.09076233 +.00000000 +00000-0 +54352-4 0 00005
2 04327 99.2712 337.1965 0003973 258.1526 112.5783 13.58725616 04
| Epoch (UTC): | 01 February 2026 02:10:41 |
| Eccentricity: | 0.0003973 |
| inclination: | 99.2712° |
| perigee height: | 1037 km |
| apogee height: | 1043 km |
| right ascension of ascending node: | 337.1965° |
| argument of perigee: | 258.1526° |
| revolutions per day: | 13.58725616 |
| mean anomaly at epoch: | 112.5783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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