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 64689U 26145.22287161 +.00000000 +00000-0 +64015-3 0 00002
2 64689 53.1601 130.6997 0000951 86.9623 273.1488 15.34405891 08
| Epoch (UTC): | 25 May 2026 05:20:56 |
| Eccentricity: | 0.0000951 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.6997° |
| argument of perigee: | 86.9623° |
| revolutions per day: | 15.34405891 |
| mean anomaly at epoch: | 273.1488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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