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 24357.83322753 .00003890 00000-0 51530-3 0 9990
2 33499 98.1274 261.6613 0006896 239.0819 120.9715 14.80476884856012
| Epoch (UTC): | 22 December 2024 19:59:50 |
| Eccentricity: | 0.0006896 |
| inclination: | 98.1274° |
| perigee height: | 623 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 261.6613° |
| argument of perigee: | 239.0819° |
| revolutions per day: | 14.80476884 |
| mean anomaly at epoch: | 120.9715° |
| orbit number at epoch: | 85601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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