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 20571U 26087.93352483 +.00000000 +00000-0 +25733-3 0 00001
2 20571 22.7420 32.4575 0468819 123.6115 240.9982 14.22103379 01
| Epoch (UTC): | 28 March 2026 22:24:16 |
| Eccentricity: | 0.0468819 |
| inclination: | 22.7420° |
| perigee height: | 481 km |
| apogee height: | 1156 km |
| right ascension of ascending node: | 32.4575° |
| argument of perigee: | 123.6115° |
| revolutions per day: | 14.22103379 |
| mean anomaly at epoch: | 240.9982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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