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 51629U 26145.40952037 +.00000000 +00000-0 +34651-4 0 00007
2 51629 87.8849 40.8089 0001810 78.1807 281.9524 13.10370543 07
| Epoch (UTC): | 25 May 2026 09:49:42 |
| Eccentricity: | 0.0001810 |
| inclination: | 87.8849° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8089° |
| argument of perigee: | 78.1807° |
| revolutions per day: | 13.10370543 |
| mean anomaly at epoch: | 281.9524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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