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 63126U 26144.72531595 +.00000000 +00000-0 +15181-4 0 00005
2 63126 97.3499 259.7871 0001775 62.0103 298.1313 15.21596035 06
| Epoch (UTC): | 24 May 2026 17:24:27 |
| Eccentricity: | 0.0001775 |
| inclination: | 97.3499° |
| perigee height: | 500 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 259.7871° |
| argument of perigee: | 62.0103° |
| revolutions per day: | 15.21596035 |
| mean anomaly at epoch: | 298.1313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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