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 23277.62954696 .00006347 00000-0 79082-3 0 9995
2 33498 98.1236 182.2449 0010653 151.4199 208.7600 14.82778781791624
| Epoch (UTC): | 04 October 2023 15:06:32 |
| Eccentricity: | 0.0010653 |
| inclination: | 98.1236° |
| perigee height: | 613 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 182.2449° |
| argument of perigee: | 151.4199° |
| revolutions per day: | 14.82778781 |
| mean anomaly at epoch: | 208.7600° |
| orbit number at epoch: | 79162 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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