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 43477U 18047B 26103.04560182 +.00002576 00000-0 +69167-4 0 09
2 43477 88.9952 206.8946 0010861 21.0069 54.8131 15.37815667439790
| Epoch (UTC): | 13 April 2026 01:05:39 |
| Eccentricity: | 0.0010861 |
| inclination: | 88.9952° |
| perigee height: | 445 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 206.8946° |
| argument of perigee: | 21.0069° |
| revolutions per day: | 15.37815667 |
| mean anomaly at epoch: | 54.8131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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