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 50174U 26145.03669992 +.00000000 +00000-0 +62046-4 0 00004
2 50174 53.2158 261.9949 0001199 88.8016 271.3113 15.08837385 00
| Epoch (UTC): | 25 May 2026 00:52:50 |
| Eccentricity: | 0.0001199 |
| inclination: | 53.2158° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 261.9949° |
| argument of perigee: | 88.8016° |
| revolutions per day: | 15.08837385 |
| mean anomaly at epoch: | 271.3113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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