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 63727U 26145.31219594 +.00000000 +00000-0 +22422-3 0 00005
2 63727 51.9004 111.8339 0000756 46.2649 313.8376 14.79950642 09
| Epoch (UTC): | 25 May 2026 07:29:33 |
| Eccentricity: | 0.0000756 |
| inclination: | 51.9004° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 111.8339° |
| argument of perigee: | 46.2649° |
| revolutions per day: | 14.79950642 |
| mean anomaly at epoch: | 313.8376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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