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 64716U 26145.32959058 +.00000000 +00000-0 +36629-3 0 00005
2 64716 69.9997 121.1005 0003886 264.4851 95.5865 14.98338149 08
| Epoch (UTC): | 25 May 2026 07:54:36 |
| Eccentricity: | 0.0003886 |
| inclination: | 69.9997° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.1005° |
| argument of perigee: | 264.4851° |
| revolutions per day: | 14.98338149 |
| mean anomaly at epoch: | 95.5865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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