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 62927U 26145.15338720 +.00000000 +00000-0 +63189-3 0 00006
2 62927 43.0035 57.2827 0001546 269.1922 90.8752 15.27598717 04
| Epoch (UTC): | 25 May 2026 03:40:52 |
| Eccentricity: | 0.0001546 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 57.2827° |
| argument of perigee: | 269.1922° |
| revolutions per day: | 15.27598717 |
| mean anomaly at epoch: | 90.8752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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