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 23155.77394587 .00000114 00000-0 47127-4 0 9994
2 07434 74.0446 172.3167 0021926 265.1998 94.6652 14.37098149549288
| Epoch (UTC): | 04 June 2023 18:34:28 |
| Eccentricity: | 0.0021926 |
| inclination: | 74.0446° |
| perigee height: | 752 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 172.3167° |
| argument of perigee: | 265.1998° |
| revolutions per day: | 14.37098149 |
| mean anomaly at epoch: | 94.6652° |
| orbit number at epoch: | 54928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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