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 24277.22099374 .00001522 00000-0 51433-3 0 9994
2 7434 74.0488 357.9371 0021185 327.8779 32.1082 14.37638995619485
| Epoch (UTC): | 03 October 2024 05:18:13 |
| Eccentricity: | 0.0021185 |
| inclination: | 74.0488° |
| perigee height: | 751 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 357.9371° |
| argument of perigee: | 327.8779° |
| revolutions per day: | 14.37638995 |
| mean anomaly at epoch: | 32.1082° |
| orbit number at epoch: | 61948 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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