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 03510U 68092A 23027.87335920 .00000218 00000-0 10543-3 0 9992
2 03510 98.4107 168.1578 0030072 359.5112 0.6035 14.27364546820820
| Epoch (UTC): | 27 January 2023 20:57:38 |
| Eccentricity: | 0.0030072 |
| inclination: | 98.4107° |
| perigee height: | 779 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 168.1578° |
| argument of perigee: | 359.5112° |
| revolutions per day: | 14.27364546 |
| mean anomaly at epoch: | 0.6035° |
| orbit number at epoch: | 82082 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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