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 51748U 26145.48049419 +.00000000 +00000-0 -95445-5 0 00008
2 51748 53.2121 324.3936 0001227 88.6546 271.4587 15.08833087 07
| Epoch (UTC): | 25 May 2026 11:31:54 |
| Eccentricity: | 0.0001227 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 324.3936° |
| argument of perigee: | 88.6546° |
| revolutions per day: | 15.08833087 |
| mean anomaly at epoch: | 271.4587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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