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 23151.52756877 .00000125 00000-0 50873-4 0 9991
2 07434 74.0448 180.1211 0021945 273.6050 86.2594 14.37096870548674
| Epoch (UTC): | 31 May 2023 12:39:41 |
| Eccentricity: | 0.0021945 |
| inclination: | 74.0448° |
| perigee height: | 752 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 180.1211° |
| argument of perigee: | 273.6050° |
| revolutions per day: | 14.37096870 |
| mean anomaly at epoch: | 86.2594° |
| orbit number at epoch: | 54867 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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