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 26157.22459382 +.00000000 +00000-0 +97346-3 0 00001
2 25544 51.6331 354.3683 0007056 137.0383 223.1158 15.49647679 06
| Epoch (UTC): | 06 June 2026 05:23:24 |
| Eccentricity: | 0.0007056 |
| inclination: | 51.6331° |
| perigee height: | 413 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 354.3683° |
| argument of perigee: | 137.0383° |
| revolutions per day: | 15.49647679 |
| mean anomaly at epoch: | 223.1158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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