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 26715U 26146.32136441 +.00000000 +00000-0 +00000-0 0 00007
2 26715 11.5199 19.9058 0038129 178.7347 10.9980 1.00278825 01
| Epoch (UTC): | 26 May 2026 07:42:45 |
| Eccentricity: | 0.0038129 |
| inclination: | 11.5199° |
| perigee height: | 35624 km |
| apogee height: | 35945 km |
| right ascension of ascending node: | 19.9058° |
| argument of perigee: | 178.7347° |
| revolutions per day: | 1.00278825 |
| mean anomaly at epoch: | 10.9980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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