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 64147U 26145.40336434 +.00000000 +00000-0 +28669-3 0 00004
2 64147 97.4466 196.7923 0001267 104.8008 255.3360 15.05655781 01
| Epoch (UTC): | 25 May 2026 09:40:50 |
| Eccentricity: | 0.0001267 |
| inclination: | 97.4466° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 196.7923° |
| argument of perigee: | 104.8008° |
| revolutions per day: | 15.05655781 |
| mean anomaly at epoch: | 255.3360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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