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 26156.33465605 +.00000000 +00000-0 +80654-4 0 00007
2 03598 34.9905 176.9892 0046597 192.5245 167.4293 14.57655349 09
| Epoch (UTC): | 05 June 2026 08:01:54 |
| Eccentricity: | 0.0046597 |
| inclination: | 34.9905° |
| perigee height: | 668 km |
| apogee height: | 734 km |
| right ascension of ascending node: | 176.9892° |
| argument of perigee: | 192.5245° |
| revolutions per day: | 14.57655349 |
| mean anomaly at epoch: | 167.4293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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