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 33499U 09002H 25143.57202200 .00001263 00000-0 16779-3 0 9997
2 33499 98.1216 55.4067 0009514 108.2480 251.9768 14.81568672878476
| Epoch (UTC): | 23 May 2025 13:43:42 |
| Eccentricity: | 0.0009514 |
| inclination: | 98.1216° |
| perigee height: | 618 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 55.4067° |
| argument of perigee: | 108.2480° |
| revolutions per day: | 14.81568672 |
| mean anomaly at epoch: | 251.9768° |
| orbit number at epoch: | 87847 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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