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 66745U 26145.62293390 +.00000000 +00000-0 +10498-3 0 00008
2 66745 97.4204 219.3812 0003741 79.5089 280.6567 15.18319763 03
| Epoch (UTC): | 25 May 2026 14:57:01 |
| Eccentricity: | 0.0003741 |
| inclination: | 97.4204° |
| perigee height: | 508 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 219.3812° |
| argument of perigee: | 79.5089° |
| revolutions per day: | 15.18319763 |
| mean anomaly at epoch: | 280.6567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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