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 26160.77141111 +.00000000 +00000-0 +14987-3 0 00003
2 25544 51.6331 336.7972 0006862 151.7869 208.3493 15.49688427 00
| Epoch (UTC): | 09 June 2026 18:30:49 |
| Eccentricity: | 0.0006862 |
| inclination: | 51.6331° |
| perigee height: | 413 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 336.7972° |
| argument of perigee: | 151.7869° |
| revolutions per day: | 15.49688427 |
| mean anomaly at epoch: | 208.3493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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