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 65563U 26145.11092220 +.00000000 +00000-0 +00000-0 0 00003
2 65563 19.9446 232.0329 0007742 208.7899 151.1988 5.31206831 06
| Epoch (UTC): | 25 May 2026 02:39:43 |
| Eccentricity: | 0.0007742 |
| inclination: | 19.9446° |
| perigee height: | 7486 km |
| apogee height: | 7507 km |
| right ascension of ascending node: | 232.0329° |
| argument of perigee: | 208.7899° |
| revolutions per day: | 5.31206831 |
| mean anomaly at epoch: | 151.1988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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