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 62764U 26145.46568106 +.00000000 +00000-0 +83498-3 0 00007
2 62764 53.1587 325.2907 0002004 83.7781 276.3448 15.31722856 08
| Epoch (UTC): | 25 May 2026 11:10:34 |
| Eccentricity: | 0.0002004 |
| inclination: | 53.1587° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 325.2907° |
| argument of perigee: | 83.7781° |
| revolutions per day: | 15.31722856 |
| mean anomaly at epoch: | 276.3448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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