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 07434U 74071B 23160.71644618 .00000152 00000-0 59815-4 0 9996
2 07434 74.0442 163.2327 0021900 255.3736 104.4989 14.37100055549995
| Epoch (UTC): | 09 June 2023 17:11:40 |
| Eccentricity: | 0.0021900 |
| inclination: | 74.0442° |
| perigee height: | 752 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 163.2327° |
| argument of perigee: | 255.3736° |
| revolutions per day: | 14.37100055 |
| mean anomaly at epoch: | 104.4989° |
| orbit number at epoch: | 54999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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