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 66042U 26145.42065289 +.00000000 +00000-0 +19754-3 0 00004
2 66042 89.0035 45.4149 0002146 69.2625 290.8756 13.51009363 03
| Epoch (UTC): | 25 May 2026 10:05:44 |
| Eccentricity: | 0.0002146 |
| inclination: | 89.0035° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.4149° |
| argument of perigee: | 69.2625° |
| revolutions per day: | 13.51009363 |
| mean anomaly at epoch: | 290.8756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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