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 40011U 26118.47615016 +.00000000 +00000-0 +23361-3 0 00005
2 40011 97.5461 305.7019 0025135 109.1841 251.2100 14.88007390 06
| Epoch (UTC): | 28 April 2026 11:25:39 |
| Eccentricity: | 0.0025135 |
| inclination: | 97.5461° |
| perigee height: | 587 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 305.7019° |
| argument of perigee: | 109.1841° |
| revolutions per day: | 14.88007390 |
| mean anomaly at epoch: | 251.2100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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