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 59U 60013B 24263.05446067 .00000183 00000-0 12937-3 0 9990
2 59 28.2471 152.0897 0188817 15.1638 345.4474 13.53090345157815
| Epoch (UTC): | 19 September 2024 01:18:25 |
| Eccentricity: | 0.0188817 |
| inclination: | 28.2471° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 152.0897° |
| argument of perigee: | 15.1638° |
| revolutions per day: | 13.53090345 |
| mean anomaly at epoch: | 345.4474° |
| orbit number at epoch: | 15781 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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