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 56747U 26145.63012176 +.00000000 +00000-0 +46574-3 0 00005
2 56747 97.5084 354.0301 0005231 77.1977 282.9856 15.46820739 04
| Epoch (UTC): | 25 May 2026 15:07:22 |
| Eccentricity: | 0.0005231 |
| inclination: | 97.5084° |
| perigee height: | 422 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 354.0301° |
| argument of perigee: | 77.1977° |
| revolutions per day: | 15.46820739 |
| mean anomaly at epoch: | 282.9856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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