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 51754U 26145.50623490 +.00000000 +00000-0 +10108-3 0 00005
2 51754 53.2143 324.0350 0001479 95.5759 264.5402 15.08825947 02
| Epoch (UTC): | 25 May 2026 12:08:58 |
| Eccentricity: | 0.0001479 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 324.0350° |
| argument of perigee: | 95.5759° |
| revolutions per day: | 15.08825947 |
| mean anomaly at epoch: | 264.5402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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