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 51966U 26145.42747814 +.00000000 +00000-0 +71829-4 0 00006
2 51966 53.1611 40.0746 0001355 85.6283 274.4873 15.31698542 02
| Epoch (UTC): | 25 May 2026 10:15:34 |
| Eccentricity: | 0.0001355 |
| inclination: | 53.1611° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 40.0746° |
| argument of perigee: | 85.6283° |
| revolutions per day: | 15.31698542 |
| mean anomaly at epoch: | 274.4873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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