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 64491U 26145.32262623 +.00000000 +00000-0 +10168-2 0 00009
2 64491 53.1606 118.5443 0001013 81.3782 278.7336 15.35412154 04
| Epoch (UTC): | 25 May 2026 07:44:34 |
| Eccentricity: | 0.0001013 |
| inclination: | 53.1606° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 118.5443° |
| argument of perigee: | 81.3782° |
| revolutions per day: | 15.35412154 |
| mean anomaly at epoch: | 278.7336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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