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 00059U 26158.69906360 +.00000000 +00000-0 +39164-4 0 00005
2 00059 28.2470 172.2750 0188765 236.1891 122.0550 13.53169726 06
| Epoch (UTC): | 07 June 2026 16:46:39 |
| Eccentricity: | 0.0188765 |
| inclination: | 28.2470° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 172.2750° |
| argument of perigee: | 236.1891° |
| revolutions per day: | 13.53169726 |
| mean anomaly at epoch: | 122.0550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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