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 64715U 26145.34628770 +.00000000 +00000-0 +35034-3 0 00009
2 64715 69.9999 121.1603 0004107 267.3195 92.7494 14.98339317 08
| Epoch (UTC): | 25 May 2026 08:18:39 |
| Eccentricity: | 0.0004107 |
| inclination: | 69.9999° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.1603° |
| argument of perigee: | 267.3195° |
| revolutions per day: | 14.98339317 |
| mean anomaly at epoch: | 92.7494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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