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 64478U 26145.32301753 +.00000000 +00000-0 +53610-3 0 00002
2 64478 53.1604 120.6781 0000979 71.6395 288.4712 15.30212006 03
| Epoch (UTC): | 25 May 2026 07:45:08 |
| Eccentricity: | 0.0000979 |
| inclination: | 53.1604° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.6781° |
| argument of perigee: | 71.6395° |
| revolutions per day: | 15.30212006 |
| mean anomaly at epoch: | 288.4712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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