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 51757U 26145.49984479 +.00000000 +00000-0 -15377-4 0 00008
2 51757 53.2127 324.3154 0001444 87.6279 272.4878 15.08844797 02
| Epoch (UTC): | 25 May 2026 11:59:46 |
| Eccentricity: | 0.0001444 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 324.3154° |
| argument of perigee: | 87.6279° |
| revolutions per day: | 15.08844797 |
| mean anomaly at epoch: | 272.4878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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