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 25544U 98067A 23332.18429367 .00024930 00000-0 44548-3 0 9999
2 25544 51.6429 236.2594 0001284 214.9817 298.9925 15.49868543427221
| Epoch (UTC): | 28 November 2023 04:25:22 |
| Eccentricity: | 0.0001284 |
| inclination: | 51.6429° |
| perigee height: | 416 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 236.2594° |
| argument of perigee: | 214.9817° |
| revolutions per day: | 15.49868543 |
| mean anomaly at epoch: | 298.9925° |
| orbit number at epoch: | 42722 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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