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 68126U 26145.49069828 +.00000000 +00000-0 +00000-0 0 00000
2 68126 0.0123 8.7030 0001421 60.6170 240.4140 1.00271751 06
| Epoch (UTC): | 25 May 2026 11:46:36 |
| Eccentricity: | 0.0001421 |
| inclination: | 0.0123° |
| perigee height: | 35781 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 8.7030° |
| argument of perigee: | 60.6170° |
| revolutions per day: | 1.00271751 |
| mean anomaly at epoch: | 240.4140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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