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 68351U 26145.25658943 +.00000000 +00000-0 +77082-4 0 00004
2 68351 54.9795 129.7242 0009738 55.1745 305.0168 14.72493622 08
| Epoch (UTC): | 25 May 2026 06:09:29 |
| Eccentricity: | 0.0009738 |
| inclination: | 54.9795° |
| perigee height: | 646 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 129.7242° |
| argument of perigee: | 55.1745° |
| revolutions per day: | 14.72493622 |
| mean anomaly at epoch: | 305.0168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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