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 64814U 26145.42781486 +.00000000 +00000-0 +18168-3 0 00001
2 64814 70.0005 300.8745 0002856 265.0855 94.9978 14.98334727 00
| Epoch (UTC): | 25 May 2026 10:16:03 |
| Eccentricity: | 0.0002856 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.8745° |
| argument of perigee: | 265.0855° |
| revolutions per day: | 14.98334727 |
| mean anomaly at epoch: | 94.9978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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