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 64720U 26145.35046156 +.00000000 +00000-0 +28720-3 0 00002
2 64720 70.0000 121.1728 0003931 265.8593 94.2116 14.98338174 05
| Epoch (UTC): | 25 May 2026 08:24:39 |
| Eccentricity: | 0.0003931 |
| inclination: | 70.0000° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.1728° |
| argument of perigee: | 265.8593° |
| revolutions per day: | 14.98338174 |
| mean anomaly at epoch: | 94.2116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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