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 64311U 26145.58298554 +.00000000 +00000-0 -11971-1 0 00003
2 64311 70.0024 0.6846 0001358 86.9335 273.1979 14.97824836 05
| Epoch (UTC): | 25 May 2026 13:59:29 |
| Eccentricity: | 0.0001358 |
| inclination: | 70.0024° |
| perigee height: | 573 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 0.6846° |
| argument of perigee: | 86.9335° |
| revolutions per day: | 14.97824836 |
| mean anomaly at epoch: | 273.1979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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