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 64007U 26145.42604904 +.00000000 +00000-0 +97690-3 0 00001
2 64007 43.0013 284.3724 0000502 8.0692 352.0168 15.27613914 06
| Epoch (UTC): | 25 May 2026 10:13:30 |
| Eccentricity: | 0.0000502 |
| inclination: | 43.0013° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 284.3724° |
| argument of perigee: | 8.0692° |
| revolutions per day: | 15.27613914 |
| mean anomaly at epoch: | 352.0168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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