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 7434U 74071B 23150.83144105 .00000120 00000-0 49276-4 0 9999
2 7434 74.0448 181.4005 0021944 274.9926 84.8722 14.37096667548888
| Epoch (UTC): | 30 May 2023 19:57:16 |
| Eccentricity: | 0.0021944 |
| inclination: | 74.0448° |
| perigee height: | 752 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 181.4005° |
| argument of perigee: | 274.9926° |
| revolutions per day: | 14.37096667 |
| mean anomaly at epoch: | 84.8722° |
| orbit number at epoch: | 54888 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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