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 64430U 26145.51040907 +.00000000 +00000-0 +15611-3 0 00001
2 64430 70.0009 240.7885 0003545 269.9327 90.1426 14.98335690 04
| Epoch (UTC): | 25 May 2026 12:14:59 |
| Eccentricity: | 0.0003545 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 240.7885° |
| argument of perigee: | 269.9327° |
| revolutions per day: | 14.98335690 |
| mean anomaly at epoch: | 90.1426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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