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 66547U 26145.75299911 +.00000000 +00000-0 +37709-3 0 00001
2 66547 51.7977 284.4879 0008933 179.7729 180.3253 15.15476822 06
| Epoch (UTC): | 25 May 2026 18:04:19 |
| Eccentricity: | 0.0008933 |
| inclination: | 51.7977° |
| perigee height: | 513 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 284.4879° |
| argument of perigee: | 179.7729° |
| revolutions per day: | 15.15476822 |
| mean anomaly at epoch: | 180.3253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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