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 64810U 26145.42347617 +.00000000 +00000-0 +23434-3 0 00003
2 64810 70.0015 300.8698 0002356 255.8930 104.1968 14.98341868 07
| Epoch (UTC): | 25 May 2026 10:09:48 |
| Eccentricity: | 0.0002356 |
| inclination: | 70.0015° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.8698° |
| argument of perigee: | 255.8930° |
| revolutions per day: | 14.98341868 |
| mean anomaly at epoch: | 104.1968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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