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 33603U 99025DCL 24357.66876376 .00002775 00000-0 25920-3 0 9992
2 33603 98.8026 254.0837 0228040 115.0821 247.4242 14.77475354936126
| Epoch (UTC): | 22 December 2024 16:03:01 |
| Eccentricity: | 0.0228040 |
| inclination: | 98.8026° |
| perigee height: | 477 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 254.0837° |
| argument of perigee: | 115.0821° |
| revolutions per day: | 14.77475354 |
| mean anomaly at epoch: | 247.4242° |
| orbit number at epoch: | 93612 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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