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 59341U 26145.21578845 +.00000000 +00000-0 -27558-4 0 00005
2 59341 43.0003 122.5984 0000943 258.8305 101.2440 15.27584059 00
| Epoch (UTC): | 25 May 2026 05:10:44 |
| Eccentricity: | 0.0000943 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 122.5984° |
| argument of perigee: | 258.8305° |
| revolutions per day: | 15.27584059 |
| mean anomaly at epoch: | 101.2440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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