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 15543U 26138.52881372 +.00000000 +00000-0 +00000-0 0 00007
2 15543 12.7100 313.8252 0132547 55.4108 316.4374 0.99806079 06
| Epoch (UTC): | 18 May 2026 12:41:29 |
| Eccentricity: | 0.0132547 |
| inclination: | 12.7100° |
| perigee height: | 35357 km |
| apogee height: | 36478 km |
| right ascension of ascending node: | 313.8252° |
| argument of perigee: | 55.4108° |
| revolutions per day: | 0.99806079 |
| mean anomaly at epoch: | 316.4374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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