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 56729U 26145.12432753 +.00000000 +00000-0 +10383-3 0 00005
2 56729 86.6559 34.9967 0002391 88.7729 271.3766 14.80237220 05
| Epoch (UTC): | 25 May 2026 02:59:01 |
| Eccentricity: | 0.0002391 |
| inclination: | 86.6559° |
| perigee height: | 627 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 34.9967° |
| argument of perigee: | 88.7729° |
| revolutions per day: | 14.80237220 |
| mean anomaly at epoch: | 271.3766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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