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 24255.52868759 .00000245 00000-0 20728-3 0 9995
2 00059 28.2482 190.7567 0188877 311.9565 46.5025 13.53088781155924
| Epoch (UTC): | 11 September 2024 12:41:18 |
| Eccentricity: | 0.0188877 |
| inclination: | 28.2482° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 190.7567° |
| argument of perigee: | 311.9565° |
| revolutions per day: | 13.53088781 |
| mean anomaly at epoch: | 46.5025° |
| orbit number at epoch: | 15592 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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