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 23157.09658728 .00000106 00000-0 44383-4 0 9993
2 7434 74.0445 169.8858 0021917 262.5611 97.3052 14.37098583549789
| Epoch (UTC): | 06 June 2023 02:19:05 |
| Eccentricity: | 0.0021917 |
| inclination: | 74.0445° |
| perigee height: | 752 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 169.8858° |
| argument of perigee: | 262.5611° |
| revolutions per day: | 14.37098583 |
| mean anomaly at epoch: | 97.3052° |
| orbit number at epoch: | 54978 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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