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 66635U 26145.29514755 +.00000000 +00000-0 +39458-3 0 00007
2 66635 53.1563 144.2234 0001037 69.1665 290.9446 15.30206520 03
| Epoch (UTC): | 25 May 2026 07:05:00 |
| Eccentricity: | 0.0001037 |
| inclination: | 53.1563° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.2234° |
| argument of perigee: | 69.1665° |
| revolutions per day: | 15.30206520 |
| mean anomaly at epoch: | 290.9446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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