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 50183U 26145.04073117 +.00000000 +00000-0 +80204-4 0 00009
2 50183 53.2127 266.3663 0001295 93.4625 266.6515 15.08831055 04
| Epoch (UTC): | 25 May 2026 00:58:39 |
| Eccentricity: | 0.0001295 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 266.3663° |
| argument of perigee: | 93.4625° |
| revolutions per day: | 15.08831055 |
| mean anomaly at epoch: | 266.6515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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