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 19120U 88039B 24282.19826534 .00001051 00000-0 52050-3 0 9999
2 19120 71.0136 82.6733 0020124 49.7725 310.5157 14.19467826885219
| Epoch (UTC): | 08 October 2024 04:45:30 |
| Eccentricity: | 0.0020124 |
| inclination: | 71.0136° |
| perigee height: | 812 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 82.6733° |
| argument of perigee: | 49.7725° |
| revolutions per day: | 14.19467826 |
| mean anomaly at epoch: | 310.5157° |
| orbit number at epoch: | 88521 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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