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 64124U 26145.58153131 +.00000000 +00000-0 +12384-2 0 00005
2 64124 43.0029 230.2393 0002138 257.7944 102.2684 15.70861781 08
| Epoch (UTC): | 25 May 2026 13:57:24 |
| Eccentricity: | 0.0002138 |
| inclination: | 43.0029° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 230.2393° |
| argument of perigee: | 257.7944° |
| revolutions per day: | 15.70861781 |
| mean anomaly at epoch: | 102.2684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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