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 64163U 26145.56673625 +.00000000 +00000-0 +40482-3 0 00002
2 64163 97.4479 196.8891 0001235 101.1073 259.0293 15.05660825 06
| Epoch (UTC): | 25 May 2026 13:36:06 |
| Eccentricity: | 0.0001235 |
| inclination: | 97.4479° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 196.8891° |
| argument of perigee: | 101.1073° |
| revolutions per day: | 15.05660825 |
| mean anomaly at epoch: | 259.0293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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