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 66758U 26145.16031043 +.00000000 +00000-0 +23604-3 0 00009
2 66758 97.4191 219.2042 0002397 76.0714 284.0788 15.19997369 07
| Epoch (UTC): | 25 May 2026 03:50:50 |
| Eccentricity: | 0.0002397 |
| inclination: | 97.4191° |
| perigee height: | 504 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 219.2042° |
| argument of perigee: | 76.0714° |
| revolutions per day: | 15.19997369 |
| mean anomaly at epoch: | 284.0788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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