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 50203U 26145.32965737 +.00000000 +00000-0 -86992-5 0 00003
2 50203 53.2135 255.1573 0001268 90.1172 269.9965 15.08833484 06
| Epoch (UTC): | 25 May 2026 07:54:42 |
| Eccentricity: | 0.0001268 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 255.1573° |
| argument of perigee: | 90.1172° |
| revolutions per day: | 15.08833484 |
| mean anomaly at epoch: | 269.9965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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