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 68427U 26145.57925051 +.00000000 +00000-0 +40951-3 0 00004
2 68427 97.4528 104.4232 0003741 78.4036 281.7618 15.18916667 06
| Epoch (UTC): | 25 May 2026 13:54:07 |
| Eccentricity: | 0.0003741 |
| inclination: | 97.4528° |
| perigee height: | 507 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 104.4232° |
| argument of perigee: | 78.4036° |
| revolutions per day: | 15.18916667 |
| mean anomaly at epoch: | 281.7618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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