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 64136U 26145.30065616 +.00000000 +00000-0 +70512-3 0 00006
2 64136 43.0010 4.9032 0000853 277.9673 82.1082 15.27599137 05
| Epoch (UTC): | 25 May 2026 07:12:56 |
| Eccentricity: | 0.0000853 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 4.9032° |
| argument of perigee: | 277.9673° |
| revolutions per day: | 15.27599137 |
| mean anomaly at epoch: | 82.1082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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