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 40055U 26145.25190848 +.00000000 +00000-0 +10956-3 0 00006
2 40055 98.3152 19.7202 0014140 85.2781 275.0045 14.81214595 09
| Epoch (UTC): | 25 May 2026 06:02:44 |
| Eccentricity: | 0.0014140 |
| inclination: | 98.3152° |
| perigee height: | 616 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 19.7202° |
| argument of perigee: | 85.2781° |
| revolutions per day: | 14.81214595 |
| mean anomaly at epoch: | 275.0045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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