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 62153U 26144.96900586 +.00000000 +00000-0 +43659-3 0 00000
2 62153 43.0027 87.5131 0001397 255.6880 104.3817 15.27589207 04
| Epoch (UTC): | 24 May 2026 23:15:22 |
| Eccentricity: | 0.0001397 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.5131° |
| argument of perigee: | 255.6880° |
| revolutions per day: | 15.27589207 |
| mean anomaly at epoch: | 104.3817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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