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 15752U 26129.31740698 +.00000000 +00000-0 +87047-4 0 00001
2 15752 82.9500 70.3219 0025395 95.3480 265.0573 13.73357493 04
| Epoch (UTC): | 09 May 2026 07:37:03 |
| Eccentricity: | 0.0025395 |
| inclination: | 82.9500° |
| perigee height: | 969 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 70.3219° |
| argument of perigee: | 95.3480° |
| revolutions per day: | 13.73357493 |
| mean anomaly at epoch: | 265.0573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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