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 20565U 26087.92280869 +.00000000 +00000-0 +32650-3 0 00007
2 20565 89.9066 245.7720 0052104 154.6747 205.7053 14.89169954 09
| Epoch (UTC): | 28 March 2026 22:08:50 |
| Eccentricity: | 0.0052104 |
| inclination: | 89.9066° |
| perigee height: | 564 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 245.7720° |
| argument of perigee: | 154.6747° |
| revolutions per day: | 14.89169954 |
| mean anomaly at epoch: | 205.7053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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