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 59327U 26145.33581350 +.00000000 +00000-0 -53681-4 0 00003
2 59327 42.9996 114.0002 0001147 260.9687 99.1035 15.27584349 01
| Epoch (UTC): | 25 May 2026 08:03:34 |
| Eccentricity: | 0.0001147 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.0002° |
| argument of perigee: | 260.9687° |
| revolutions per day: | 15.27584349 |
| mean anomaly at epoch: | 99.1035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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