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 26145.36779345 +.00000000 +00000-0 +00000-0 0 00006
2 26715 11.5190 19.9120 0038129 178.8543 26.6256 1.00278265 09
| Epoch (UTC): | 25 May 2026 08:49:37 |
| Eccentricity: | 0.0038129 |
| inclination: | 11.5190° |
| perigee height: | 35624 km |
| apogee height: | 35946 km |
| right ascension of ascending node: | 19.9120° |
| argument of perigee: | 178.8543° |
| revolutions per day: | 1.00278265 |
| mean anomaly at epoch: | 26.6256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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