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 19112U 76126BZ 24357.53347494 .00002468 00000-0 57347-3 0 9995
2 19112 65.8221 182.7815 0922130 335.6076 20.3802 13.20911878629045
| Epoch (UTC): | 22 December 2024 12:48:12 |
| Eccentricity: | 0.0922130 |
| inclination: | 65.8221° |
| perigee height: | 484 km |
| apogee height: | 1878 km |
| right ascension of ascending node: | 182.7815° |
| argument of perigee: | 335.6076° |
| revolutions per day: | 13.20911878 |
| mean anomaly at epoch: | 20.3802° |
| orbit number at epoch: | 62904 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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