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 59343U 26145.60552475 +.00000000 +00000-0 +24897-4 0 00003
2 59343 98.8199 153.7754 0002038 86.6647 273.4759 14.13325003 01
| Epoch (UTC): | 25 May 2026 14:31:57 |
| Eccentricity: | 0.0002038 |
| inclination: | 98.8199° |
| perigee height: | 847 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 153.7754° |
| argument of perigee: | 86.6647° |
| revolutions per day: | 14.13325003 |
| mean anomaly at epoch: | 273.4759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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