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 64832U 26145.44289954 +.00000000 +00000-0 +11972-3 0 00002
2 64832 51.9014 318.7032 0000753 131.3564 228.7463 14.79935578 07
| Epoch (UTC): | 25 May 2026 10:37:46 |
| Eccentricity: | 0.0000753 |
| inclination: | 51.9014° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 318.7032° |
| argument of perigee: | 131.3564° |
| revolutions per day: | 14.79935578 |
| mean anomaly at epoch: | 228.7463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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