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 00058U 26100.12279939 +.00000000 +00000-0 +33053-4 0 00005
2 00058 28.3260 125.1012 0164886 4.2175 355.9727 13.46428099 04
| Epoch (UTC): | 10 April 2026 02:56:49 |
| Eccentricity: | 0.0164886 |
| inclination: | 28.3260° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 125.1012° |
| argument of perigee: | 4.2175° |
| revolutions per day: | 13.46428099 |
| mean anomaly at epoch: | 355.9727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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