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 43186U 26139.49571269 +.00000000 +00000-0 +16676-3 0 00008
2 43186 97.5385 44.4689 0009960 112.9463 247.2822 15.16369820 04
| Epoch (UTC): | 19 May 2026 11:53:49 |
| Eccentricity: | 0.0009960 |
| inclination: | 97.5385° |
| perigee height: | 510 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 44.4689° |
| argument of perigee: | 112.9463° |
| revolutions per day: | 15.16369820 |
| mean anomaly at epoch: | 247.2822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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