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 43184U 26145.52991501 +.00000000 +00000-0 +16731-2 0 00003
2 43184 97.4402 75.9216 0005376 143.3626 216.8018 15.94652847 01
| Epoch (UTC): | 25 May 2026 12:43:04 |
| Eccentricity: | 0.0005376 |
| inclination: | 97.4402° |
| perigee height: | 286 km |
| apogee height: | 293 km |
| right ascension of ascending node: | 75.9216° |
| argument of perigee: | 143.3626° |
| revolutions per day: | 15.94652847 |
| mean anomaly at epoch: | 216.8018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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