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 23086.73693168 .00000141 00000-0 15223-3 0 9994
2 00005 34.2607 346.3417 1846818 232.8595 108.8821 10.85075180315313
| Epoch (UTC): | 27 March 2023 17:41:10 |
| Eccentricity: | 0.1846818 |
| inclination: | 34.2607° |
| perigee height: | 648 km |
| apogee height: | 3832 km |
| right ascension of ascending node: | 346.3417° |
| argument of perigee: | 232.8595° |
| revolutions per day: | 10.85075180 |
| mean anomaly at epoch: | 108.8821° |
| orbit number at epoch: | 31531 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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