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 20511U 26135.13460200 +.00000000 +00000-0 +24037-4 0 00005
2 20511 82.5206 161.0028 0015041 229.6790 130.3111 14.82194712 07
| Epoch (UTC): | 15 May 2026 03:13:49 |
| Eccentricity: | 0.0015041 |
| inclination: | 82.5206° |
| perigee height: | 612 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 161.0028° |
| argument of perigee: | 229.6790° |
| revolutions per day: | 14.82194712 |
| mean anomaly at epoch: | 130.3111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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