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 64346U 26145.55584830 +.00000000 +00000-0 +23166-3 0 00003
2 64346 70.0006 200.7317 0003803 267.9303 92.1420 14.98335028 03
| Epoch (UTC): | 25 May 2026 13:20:25 |
| Eccentricity: | 0.0003803 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.7317° |
| argument of perigee: | 267.9303° |
| revolutions per day: | 14.98335028 |
| mean anomaly at epoch: | 92.1420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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