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 8924U 76061B 23153.19032247 .00000249 00000-0 91913-4 0 9997
2 8924 74.0591 66.8734 0013755 151.3423 11.0112 14.37507306456327
| Epoch (UTC): | 02 June 2023 04:34:03 |
| Eccentricity: | 0.0013755 |
| inclination: | 74.0591° |
| perigee height: | 757 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 66.8734° |
| argument of perigee: | 151.3423° |
| revolutions per day: | 14.37507306 |
| mean anomaly at epoch: | 11.0112° |
| orbit number at epoch: | 45632 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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