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 64050U 26145.65569506 +.00000000 +00000-0 +14944-3 0 00003
2 64050 97.3755 217.8041 0001740 218.0004 142.1109 15.19781017 01
| Epoch (UTC): | 25 May 2026 15:44:12 |
| Eccentricity: | 0.0001740 |
| inclination: | 97.3755° |
| perigee height: | 505 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 217.8041° |
| argument of perigee: | 218.0004° |
| revolutions per day: | 15.19781017 |
| mean anomaly at epoch: | 142.1109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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