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 63726U 26145.28650657 +.00000000 +00000-0 +79987-4 0 00008
2 63726 51.9017 104.3919 0000727 65.9653 294.1385 14.79934000 05
| Epoch (UTC): | 25 May 2026 06:52:34 |
| Eccentricity: | 0.0000727 |
| inclination: | 51.9017° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 104.3919° |
| argument of perigee: | 65.9653° |
| revolutions per day: | 14.79934000 |
| mean anomaly at epoch: | 294.1385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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