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 22273.98457720 .00000240 00000-0 30330-3 0 9996
2 00005 34.2438 174.1794 1846494 152.5611 218.6008 10.85013588296002
| Epoch (UTC): | 30 September 2022 23:37:47 |
| Eccentricity: | 0.1846494 |
| inclination: | 34.2438° |
| perigee height: | 649 km |
| apogee height: | 3832 km |
| right ascension of ascending node: | 174.1794° |
| argument of perigee: | 152.5611° |
| revolutions per day: | 10.85013588 |
| mean anomaly at epoch: | 218.6008° |
| orbit number at epoch: | 29600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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