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 64429U 26145.52710685 +.00000000 +00000-0 +23042-3 0 00004
2 64429 70.0008 240.8464 0002939 267.6392 92.4431 14.98335845 01
| Epoch (UTC): | 25 May 2026 12:39:02 |
| Eccentricity: | 0.0002939 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.8464° |
| argument of perigee: | 267.6392° |
| revolutions per day: | 14.98335845 |
| mean anomaly at epoch: | 92.4431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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