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 64713U 26145.30874395 +.00000000 +00000-0 +18172-3 0 00003
2 64713 70.0004 121.3977 0003991 262.2260 97.8446 14.98334732 08
| Epoch (UTC): | 25 May 2026 07:24:35 |
| Eccentricity: | 0.0003991 |
| inclination: | 70.0004° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.3977° |
| argument of perigee: | 262.2260° |
| revolutions per day: | 14.98334732 |
| mean anomaly at epoch: | 97.8446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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