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 59256U 26145.39325897 +.00000000 +00000-0 +87063-5 0 00003
2 59256 53.1604 184.6172 0001353 83.6030 276.5125 15.30194094 03
| Epoch (UTC): | 25 May 2026 09:26:17 |
| Eccentricity: | 0.0001353 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.6172° |
| argument of perigee: | 83.6030° |
| revolutions per day: | 15.30194094 |
| mean anomaly at epoch: | 276.5125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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