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 65551U 26145.36488484 +.00000000 +00000-0 +18584-3 0 00007
2 65551 49.9849 145.2838 0008618 241.0706 118.9368 14.84100249 00
| Epoch (UTC): | 25 May 2026 08:45:26 |
| Eccentricity: | 0.0008618 |
| inclination: | 49.9849° |
| perigee height: | 610 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 145.2838° |
| argument of perigee: | 241.0706° |
| revolutions per day: | 14.84100249 |
| mean anomaly at epoch: | 118.9368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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