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 00005U 58002B 23160.93351847 .00000002 00000-0 -16484-4 0 9992
2 00005 34.2502 117.6321 1846829 206.9142 142.2602 10.85082190323375
| Epoch (UTC): | 09 June 2023 22:24:15 |
| Eccentricity: | 0.1846829 |
| inclination: | 34.2502° |
| perigee height: | 648 km |
| apogee height: | 3832 km |
| right ascension of ascending node: | 117.6321° |
| argument of perigee: | 206.9142° |
| revolutions per day: | 10.85082190 |
| mean anomaly at epoch: | 142.2602° |
| orbit number at epoch: | 32337 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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