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 64141U 26145.64557904 +.00000000 +00000-0 +90550-3 0 00009
2 64141 43.0041 3.1865 0000369 269.6799 90.4011 15.27600781 01
| Epoch (UTC): | 25 May 2026 15:29:38 |
| Eccentricity: | 0.0000369 |
| inclination: | 43.0041° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 3.1865° |
| argument of perigee: | 269.6799° |
| revolutions per day: | 15.27600781 |
| mean anomaly at epoch: | 90.4011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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