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 66760U 26145.15062875 +.00000000 +00000-0 +21427-3 0 00009
2 66760 97.4193 219.2255 0001739 76.0191 284.1238 15.20028857 06
| Epoch (UTC): | 25 May 2026 03:36:54 |
| Eccentricity: | 0.0001739 |
| inclination: | 97.4193° |
| perigee height: | 505 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 219.2255° |
| argument of perigee: | 76.0191° |
| revolutions per day: | 15.20028857 |
| mean anomaly at epoch: | 284.1238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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