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 52255U 26144.97873971 +.00000000 +00000-0 +00000-0 0 00000
2 52255 0.0064 311.8341 0000683 66.4455 341.7196 1.00270188 07
| Epoch (UTC): | 24 May 2026 23:29:23 |
| Eccentricity: | 0.0000683 |
| inclination: | 0.0064° |
| perigee height: | 35784 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 311.8341° |
| argument of perigee: | 66.4455° |
| revolutions per day: | 1.00270188 |
| mean anomaly at epoch: | 341.7196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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