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 65198U 26145.32793308 +.00000000 +00000-0 +46263-3 0 00009
2 65198 53.1563 159.6158 0000979 77.1196 282.9914 15.30202339 08
| Epoch (UTC): | 25 May 2026 07:52:13 |
| Eccentricity: | 0.0000979 |
| inclination: | 53.1563° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 159.6158° |
| argument of perigee: | 77.1196° |
| revolutions per day: | 15.30202339 |
| mean anomaly at epoch: | 282.9914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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