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 23027.36389904 .00000179 00000-0 22158-3 0 9994
2 00005 34.2500 169.3514 1846156 325.4822 23.8370 10.85055487308868
| Epoch (UTC): | 27 January 2023 08:44:00 |
| Eccentricity: | 0.1846156 |
| inclination: | 34.2500° |
| perigee height: | 649 km |
| apogee height: | 3831 km |
| right ascension of ascending node: | 169.3514° |
| argument of perigee: | 325.4822° |
| revolutions per day: | 10.85055487 |
| mean anomaly at epoch: | 23.8370° |
| orbit number at epoch: | 30886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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