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 26356U 26146.28693965 +.00000000 +00000-0 +00000-0 0 00002
2 26356 13.1551 12.0135 0002185 322.5994 207.2895 1.00266485 07
| Epoch (UTC): | 26 May 2026 06:53:11 |
| Eccentricity: | 0.0002185 |
| inclination: | 13.1551° |
| perigee height: | 35779 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 12.0135° |
| argument of perigee: | 322.5994° |
| revolutions per day: | 1.00266485 |
| mean anomaly at epoch: | 207.2895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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