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 64434U 26145.51474948 +.00000000 +00000-0 +20817-3 0 00005
2 64434 70.0009 240.8000 0003544 270.7566 89.3187 14.98334605 01
| Epoch (UTC): | 25 May 2026 12:21:14 |
| Eccentricity: | 0.0003544 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 240.8000° |
| argument of perigee: | 270.7566° |
| revolutions per day: | 14.98334605 |
| mean anomaly at epoch: | 89.3187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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