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 26931U 26156.77450163 +.00000000 +00000-0 +87929-4 0 00006
2 26931 67.0513 273.7893 0006115 264.0839 95.9566 14.31951978 07
| Epoch (UTC): | 05 June 2026 18:35:16 |
| Eccentricity: | 0.0006115 |
| inclination: | 67.0513° |
| perigee height: | 781 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 273.7893° |
| argument of perigee: | 264.0839° |
| revolutions per day: | 14.31951978 |
| mean anomaly at epoch: | 95.9566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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