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 55326U 26145.29471616 +.00000000 +00000-0 +15829-3 0 00006
2 55326 40.4973 122.4144 0004522 236.1140 123.9239 15.22687898 03
| Epoch (UTC): | 25 May 2026 07:04:23 |
| Eccentricity: | 0.0004522 |
| inclination: | 40.4973° |
| perigee height: | 495 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 122.4144° |
| argument of perigee: | 236.1140° |
| revolutions per day: | 15.22687898 |
| mean anomaly at epoch: | 123.9239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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