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 64815U 26145.44451039 +.00000000 +00000-0 +30937-3 0 00000
2 64815 70.0001 300.9331 0002565 270.1634 89.9231 14.98338310 06
| Epoch (UTC): | 25 May 2026 10:40:05 |
| Eccentricity: | 0.0002565 |
| inclination: | 70.0001° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.9331° |
| argument of perigee: | 270.1634° |
| revolutions per day: | 14.98338310 |
| mean anomaly at epoch: | 89.9231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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