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 15592U 85020A 23152.43574046 .00023174 00000-0 41764-3 0 9995
2 15592 82.5302 285.8029 0007256 357.6355 2.4861 15.49613452 97199
| Epoch (UTC): | 01 June 2023 10:27:27 |
| Eccentricity: | 0.0007256 |
| inclination: | 82.5302° |
| perigee height: | 413 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 285.8029° |
| argument of perigee: | 357.6355° |
| revolutions per day: | 15.49613452 |
| mean anomaly at epoch: | 2.4861° |
| orbit number at epoch: | 9719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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