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 64746U 26145.46650594 +.00000000 +00000-0 +54157-3 0 00002
2 64746 53.1594 171.8585 0001030 76.5929 283.5186 15.30207220 08
| Epoch (UTC): | 25 May 2026 11:11:46 |
| Eccentricity: | 0.0001030 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.8585° |
| argument of perigee: | 76.5929° |
| revolutions per day: | 15.30207220 |
| mean anomaly at epoch: | 283.5186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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