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 33498U 09002G 23090.21739785 .00006224 00000-0 79979-3 0 9992
2 33498 98.1425 351.8163 0011685 51.3118 308.9137 14.81488325764287
| Epoch (UTC): | 31 March 2023 05:13:03 |
| Eccentricity: | 0.0011685 |
| inclination: | 98.1425° |
| perigee height: | 616 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 351.8163° |
| argument of perigee: | 51.3118° |
| revolutions per day: | 14.81488325 |
| mean anomaly at epoch: | 308.9137° |
| orbit number at epoch: | 76428 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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