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 55327U 26145.22915617 +.00000000 +00000-0 +19269-3 0 00006
2 55327 40.4985 124.4191 0004302 235.7086 124.3316 15.22695743 00
| Epoch (UTC): | 25 May 2026 05:29:59 |
| Eccentricity: | 0.0004302 |
| inclination: | 40.4985° |
| perigee height: | 495 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 124.4191° |
| argument of perigee: | 235.7086° |
| revolutions per day: | 15.22695743 |
| mean anomaly at epoch: | 124.3316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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