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 64809U 26145.37341198 +.00000000 +00000-0 +30221-3 0 00005
2 64809 70.0003 301.0949 0002964 265.9530 94.1290 14.98337388 05
| Epoch (UTC): | 25 May 2026 08:57:42 |
| Eccentricity: | 0.0002964 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.0949° |
| argument of perigee: | 265.9530° |
| revolutions per day: | 14.98337388 |
| mean anomaly at epoch: | 94.1290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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