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 59342U 26145.36280897 +.00000000 +00000-0 +63145-4 0 00000
2 59342 43.0032 114.1999 0000914 272.2100 87.8647 15.27572892 07
| Epoch (UTC): | 25 May 2026 08:42:26 |
| Eccentricity: | 0.0000914 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.1999° |
| argument of perigee: | 272.2100° |
| revolutions per day: | 15.27572892 |
| mean anomaly at epoch: | 87.8647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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