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 20624U 26100.06101471 +.00000000 +00000-0 +19560-3 0 00000
2 20624 71.0404 314.9743 0014308 163.8779 196.2802 14.14835009 03
| Epoch (UTC): | 10 April 2026 01:27:51 |
| Eccentricity: | 0.0014308 |
| inclination: | 71.0404° |
| perigee height: | 833 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 314.9743° |
| argument of perigee: | 163.8779° |
| revolutions per day: | 14.14835009 |
| mean anomaly at epoch: | 196.2802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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