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 18467U 78026HE 24355.51673773 .00000877 00000-0 37617-3 0 9996
2 18467 98.8556 5.1278 0093436 174.6467 337.5919 14.25040862 67352
| Epoch (UTC): | 20 December 2024 12:24:06 |
| Eccentricity: | 0.0093436 |
| inclination: | 98.8556° |
| perigee height: | 741 km |
| apogee height: | 875 km |
| right ascension of ascending node: | 5.1278° |
| argument of perigee: | 174.6467° |
| revolutions per day: | 14.25040862 |
| mean anomaly at epoch: | 337.5919° |
| orbit number at epoch: | 6735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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