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 59918U 26145.62276034 +.00000000 +00000-0 +24615-3 0 00004
2 59918 97.5833 160.9947 0010824 331.5060 28.5581 15.18817708 03
| Epoch (UTC): | 25 May 2026 14:56:46 |
| Eccentricity: | 0.0010824 |
| inclination: | 97.5833° |
| perigee height: | 502 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 160.9947° |
| argument of perigee: | 331.5060° |
| revolutions per day: | 15.18817708 |
| mean anomaly at epoch: | 28.5581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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