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 64723U 26145.58303509 +.00000000 +00000-0 +00000-0 0 00006
2 64723 0.6235 334.3445 0001456 25.1386 90.1326 1.00270016 05
| Epoch (UTC): | 25 May 2026 13:59:34 |
| Eccentricity: | 0.0001456 |
| inclination: | 0.6235° |
| perigee height: | 35781 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 334.3445° |
| argument of perigee: | 25.1386° |
| revolutions per day: | 1.00270016 |
| mean anomaly at epoch: | 90.1326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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