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 50170U 26144.74632647 +.00000000 +00000-0 +13480-4 0 00002
2 50170 53.2157 267.6888 0001324 90.4069 269.7075 15.08837785 09
| Epoch (UTC): | 24 May 2026 17:54:42 |
| Eccentricity: | 0.0001324 |
| inclination: | 53.2157° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 267.6888° |
| argument of perigee: | 90.4069° |
| revolutions per day: | 15.08837785 |
| mean anomaly at epoch: | 269.7075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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