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 68135U 26145.40818565 +.00000000 +00000-0 +90511-4 0 00001
2 68135 50.0073 137.7635 0000283 352.9118 7.1750 13.29331039 08
| Epoch (UTC): | 25 May 2026 09:47:47 |
| Eccentricity: | 0.0000283 |
| inclination: | 50.0073° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 137.7635° |
| argument of perigee: | 352.9118° |
| revolutions per day: | 13.29331039 |
| mean anomaly at epoch: | 7.1750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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