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 08924U 76061B 23150.26808248 .00000211 00000-0 79234-4 0 9995
2 08924 74.0589 72.2435 0013816 157.8137 7.9793 14.37505511455698
| Epoch (UTC): | 30 May 2023 06:26:02 |
| Eccentricity: | 0.0013816 |
| inclination: | 74.0589° |
| perigee height: | 757 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 72.2435° |
| argument of perigee: | 157.8137° |
| revolutions per day: | 14.37505511 |
| mean anomaly at epoch: | 7.9793° |
| orbit number at epoch: | 45569 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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