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 26695U 26150.39989529 +.00000000 +00000-0 +00000-0 0 00009
2 26695 12.1068 18.5845 0004062 223.0302 341.5691 0.99150986 09
| Epoch (UTC): | 30 May 2026 09:35:50 |
| Eccentricity: | 0.0004062 |
| inclination: | 12.1068° |
| perigee height: | 36087 km |
| apogee height: | 36121 km |
| right ascension of ascending node: | 18.5845° |
| argument of perigee: | 223.0302° |
| revolutions per day: | 0.99150986 |
| mean anomaly at epoch: | 341.5691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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