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 64092U 26145.59534160 +.00000000 +00000-0 +70006-3 0 00001
2 64092 97.4696 223.2761 0013029 86.5804 273.6925 15.26655413 05
| Epoch (UTC): | 25 May 2026 14:17:17 |
| Eccentricity: | 0.0013029 |
| inclination: | 97.4696° |
| perigee height: | 477 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 223.2761° |
| argument of perigee: | 86.5804° |
| revolutions per day: | 15.26655413 |
| mean anomaly at epoch: | 273.6925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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