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 23026.44305159 .00000204 00000-0 25031-3 0 9994
2 00005 34.2506 172.1896 1846235 321.3365 26.8224 10.85055309308767
| Epoch (UTC): | 26 January 2023 10:37:59 |
| Eccentricity: | 0.1846235 |
| inclination: | 34.2506° |
| perigee height: | 649 km |
| apogee height: | 3831 km |
| right ascension of ascending node: | 172.1896° |
| argument of perigee: | 321.3365° |
| revolutions per day: | 10.85055309 |
| mean anomaly at epoch: | 26.8224° |
| orbit number at epoch: | 30876 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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