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 55508U 26144.97405737 +.00000000 +00000-0 +00000-0 0 00005
2 55508 0.0435 42.5068 0005393 10.6450 119.0817 1.00270250 02
| Epoch (UTC): | 24 May 2026 23:22:38 |
| Eccentricity: | 0.0005393 |
| inclination: | 0.0435° |
| perigee height: | 35764 km |
| apogee height: | 35810 km |
| right ascension of ascending node: | 42.5068° |
| argument of perigee: | 10.6450° |
| revolutions per day: | 1.00270250 |
| mean anomaly at epoch: | 119.0817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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