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 23158.26517274 -.00000016 00000-0 -35848-4 0 9994
2 00005 34.2474 125.8582 1846709 194.8971 158.9112 10.85082185323087
| Epoch (UTC): | 07 June 2023 06:21:50 |
| Eccentricity: | 0.1846709 |
| inclination: | 34.2474° |
| perigee height: | 649 km |
| apogee height: | 3832 km |
| right ascension of ascending node: | 125.8582° |
| argument of perigee: | 194.8971° |
| revolutions per day: | 10.85082185 |
| mean anomaly at epoch: | 158.9112° |
| orbit number at epoch: | 32308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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