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 66954U 26145.39384397 +.00000000 +00000-0 +34733-4 0 00001
2 66954 86.4931 290.0925 0001511 113.5058 246.6235 13.24427946 01
| Epoch (UTC): | 25 May 2026 09:27:08 |
| Eccentricity: | 0.0001511 |
| inclination: | 86.4931° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 290.0925° |
| argument of perigee: | 113.5058° |
| revolutions per day: | 13.24427946 |
| mean anomaly at epoch: | 246.6235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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