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 62562U 26145.59707941 +.00000000 +00000-0 +15055-2 0 00002
2 62562 43.0005 36.7047 0001779 264.0320 96.0344 15.70859887 07
| Epoch (UTC): | 25 May 2026 14:19:47 |
| Eccentricity: | 0.0001779 |
| inclination: | 43.0005° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 36.7047° |
| argument of perigee: | 264.0320° |
| revolutions per day: | 15.70859887 |
| mean anomaly at epoch: | 96.0344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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