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 64372U 26145.24037065 +.00000000 +00000-0 +15331-2 0 00005
2 64372 42.9998 342.9528 0001409 288.7570 71.3145 15.70901552 05
| Epoch (UTC): | 25 May 2026 05:46:08 |
| Eccentricity: | 0.0001409 |
| inclination: | 42.9998° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 342.9528° |
| argument of perigee: | 288.7570° |
| revolutions per day: | 15.70901552 |
| mean anomaly at epoch: | 71.3145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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