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 64673U 26145.27959437 +.00000000 +00000-0 +70274-3 0 00006
2 64673 53.1602 130.3511 0001113 79.9608 280.1521 15.34393817 07
| Epoch (UTC): | 25 May 2026 06:42:36 |
| Eccentricity: | 0.0001113 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.3511° |
| argument of perigee: | 79.9608° |
| revolutions per day: | 15.34393817 |
| mean anomaly at epoch: | 280.1521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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