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 15593U 85020B 24284.49502693 .00002183 00000-0 24770-3 0 9993
2 15593 82.5342 280.7313 0010615 200.5838 159.4952 14.85894038140855
| Epoch (UTC): | 10 October 2024 11:52:50 |
| Eccentricity: | 0.0010615 |
| inclination: | 82.5342° |
| perigee height: | 603 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 280.7313° |
| argument of perigee: | 200.5838° |
| revolutions per day: | 14.85894038 |
| mean anomaly at epoch: | 159.4952° |
| orbit number at epoch: | 14085 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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