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 59329U 26145.40890486 +.00000000 +00000-0 +31772-4 0 00002
2 59329 43.0005 113.6889 0001122 270.3893 89.6830 15.27582554 04
| Epoch (UTC): | 25 May 2026 09:48:49 |
| Eccentricity: | 0.0001122 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.6889° |
| argument of perigee: | 270.3893° |
| revolutions per day: | 15.27582554 |
| mean anomaly at epoch: | 89.6830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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