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 28522U 26039.29954111 +.00000000 +00000-0 +84467-4 0 00007
2 28522 82.9468 119.7470 0044255 238.7371 120.9455 13.90046069 02
| Epoch (UTC): | 08 February 2026 07:11:20 |
| Eccentricity: | 0.0044255 |
| inclination: | 82.9468° |
| perigee height: | 896 km |
| apogee height: | 961 km |
| right ascension of ascending node: | 119.7470° |
| argument of perigee: | 238.7371° |
| revolutions per day: | 13.90046069 |
| mean anomaly at epoch: | 120.9455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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