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 25544U 26110.13518309 +.00000000 +00000-0 +15272-3 0 00003
2 25544 51.6328 227.4156 0006665 328.2959 31.7627 15.48842238 06
| Epoch (UTC): | 20 April 2026 03:14:39 |
| Eccentricity: | 0.0006665 |
| inclination: | 51.6328° |
| perigee height: | 416 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 227.4156° |
| argument of perigee: | 328.2959° |
| revolutions per day: | 15.48842238 |
| mean anomaly at epoch: | 31.7627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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