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 62757U 26144.65272970 +.00000000 +00000-0 +92998-3 0 00005
2 62757 42.9991 253.8652 0002034 273.4559 86.6078 15.76418227 06
| Epoch (UTC): | 24 May 2026 15:39:55 |
| Eccentricity: | 0.0002034 |
| inclination: | 42.9991° |
| perigee height: | 339 km |
| apogee height: | 342 km |
| right ascension of ascending node: | 253.8652° |
| argument of perigee: | 273.4559° |
| revolutions per day: | 15.76418227 |
| mean anomaly at epoch: | 86.6078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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