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 data is extracted from the following two-line orbital elements,
1 20774U 90078A 24277.57289725 .00008496 00000-0 62886-3 0 9991
2 20774 82.9461 196.5097 0770396 211.0751 144.2624 13.83571647686332
| Epoch (UTC): | 03 October 2024 13:44:58 |
| Eccentricity: | 0.0770396 |
| inclination: | 82.9461° |
| perigee height: | 386 km |
| apogee height: | 1516 km |
| right ascension of ascending node: | 196.5097° |
| argument of perigee: | 211.0751° |
| revolutions per day: | 13.83571647 |
| mean anomaly at epoch: | 144.2624° |
| orbit number at epoch: | 68633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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