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 61564U 26145.55055318 +.00000000 +00000-0 +19490-3 0 00001
2 61564 88.9815 63.4967 0004886 277.7567 82.3033 13.58032392 00
| Epoch (UTC): | 25 May 2026 13:12:47 |
| Eccentricity: | 0.0004886 |
| inclination: | 88.9815° |
| perigee height: | 1039 km |
| apogee height: | 1046 km |
| right ascension of ascending node: | 63.4967° |
| argument of perigee: | 277.7567° |
| revolutions per day: | 13.58032392 |
| mean anomaly at epoch: | 82.3033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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