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 03598U 26162.22530439 +.00000000 +00000-0 +74210-4 0 00001
2 03598 34.9910 143.5450 0047034 240.1708 119.4305 14.57660183 09
| Epoch (UTC): | 11 June 2026 05:24:26 |
| Eccentricity: | 0.0047034 |
| inclination: | 34.9910° |
| perigee height: | 667 km |
| apogee height: | 734 km |
| right ascension of ascending node: | 143.5450° |
| argument of perigee: | 240.1708° |
| revolutions per day: | 14.57660183 |
| mean anomaly at epoch: | 119.4305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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