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 51958U 26145.66002235 +.00000000 +00000-0 +24313-3 0 00009
2 51958 53.1591 15.5676 0001360 83.6753 276.4404 15.31724991 05
| Epoch (UTC): | 25 May 2026 15:50:25 |
| Eccentricity: | 0.0001360 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 15.5676° |
| argument of perigee: | 83.6753° |
| revolutions per day: | 15.31724991 |
| mean anomaly at epoch: | 276.4404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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