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 15032U 84056B 24357.75836671 .00000539 00000-0 19495-3 0 9996
2 15032 74.0701 95.1798 0018233 284.3352 75.5776 14.35760851120476
| Epoch (UTC): | 22 December 2024 18:12:02 |
| Eccentricity: | 0.0018233 |
| inclination: | 74.0701° |
| perigee height: | 759 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 95.1798° |
| argument of perigee: | 284.3352° |
| revolutions per day: | 14.35760851 |
| mean anomaly at epoch: | 75.5776° |
| orbit number at epoch: | 12047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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