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 50171U 26145.35721029 +.00000000 +00000-0 +29081-4 0 00008
2 50171 53.2166 264.9472 0001132 94.6385 265.4736 15.08834045 06
| Epoch (UTC): | 25 May 2026 08:34:22 |
| Eccentricity: | 0.0001132 |
| inclination: | 53.2166° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 264.9472° |
| argument of perigee: | 94.6385° |
| revolutions per day: | 15.08834045 |
| mean anomaly at epoch: | 265.4736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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