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 64798U 26145.39010845 +.00000000 +00000-0 +27369-3 0 00005
2 64798 70.0001 301.1547 0003011 265.7214 94.3601 14.98338188 03
| Epoch (UTC): | 25 May 2026 09:21:45 |
| Eccentricity: | 0.0003011 |
| inclination: | 70.0001° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.1547° |
| argument of perigee: | 265.7214° |
| revolutions per day: | 14.98338188 |
| mean anomaly at epoch: | 94.3601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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