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 26108.07046200 +.00000000 +00000-0 +14069-3 0 00002
2 25544 51.6329 237.6272 0006577 320.1418 39.9086 15.48808425 01
| Epoch (UTC): | 18 April 2026 01:41:27 |
| Eccentricity: | 0.0006577 |
| inclination: | 51.6329° |
| perigee height: | 416 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 237.6272° |
| argument of perigee: | 320.1418° |
| revolutions per day: | 15.48808425 |
| mean anomaly at epoch: | 39.9086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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