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 61747U 26145.51373638 +.00000000 +00000-0 +38483-3 0 00001
2 61747 97.3037 18.5230 0009157 15.0626 345.0894 15.44664959 03
| Epoch (UTC): | 25 May 2026 12:19:46 |
| Eccentricity: | 0.0009157 |
| inclination: | 97.3037° |
| perigee height: | 426 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 18.5230° |
| argument of perigee: | 15.0626° |
| revolutions per day: | 15.44664959 |
| mean anomaly at epoch: | 345.0894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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