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 43782U 26145.58037997 +.00000000 +00000-0 +34778-3 0 00005
2 43782 97.4076 199.3161 0010570 24.9734 335.2011 15.21434682 02
| Epoch (UTC): | 25 May 2026 13:55:44 |
| Eccentricity: | 0.0010570 |
| inclination: | 97.4076° |
| perigee height: | 494 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 199.3161° |
| argument of perigee: | 24.9734° |
| revolutions per day: | 15.21434682 |
| mean anomaly at epoch: | 335.2011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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