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 64011U 26145.39663979 +.00000000 +00000-0 +78935-3 0 00000
2 64011 42.9990 285.0155 0001347 273.0527 87.0171 15.27600319 02
| Epoch (UTC): | 25 May 2026 09:31:09 |
| Eccentricity: | 0.0001347 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 285.0155° |
| argument of perigee: | 273.0527° |
| revolutions per day: | 15.27600319 |
| mean anomaly at epoch: | 87.0171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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