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 00059U 60013B 24254.86465980 .00000246 00000-0 20809-3 0 9991
2 00059 28.2482 194.1681 0188875 306.3782 51.9473 13.53088573155832
| Epoch (UTC): | 10 September 2024 20:45:06 |
| Eccentricity: | 0.0188875 |
| inclination: | 28.2482° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 194.1681° |
| argument of perigee: | 306.3782° |
| revolutions per day: | 13.53088573 |
| mean anomaly at epoch: | 51.9473° |
| orbit number at epoch: | 15583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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