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 53782U 26145.66668980 +.00000000 +00000-0 +31618-2 0 00006
2 53782 53.2165 270.8475 0001127 36.3950 108.4999 15.78284898 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001127 |
| inclination: | 53.2165° |
| perigee height: | 335 km |
| apogee height: | 336 km |
| right ascension of ascending node: | 270.8475° |
| argument of perigee: | 36.3950° |
| revolutions per day: | 15.78284898 |
| mean anomaly at epoch: | 108.4999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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