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 is defined by the following mean orbital elements,
1 46839U 20079N 23096.36045889 .08834687 23464-5 14923-2 0 9990
2 46839 97.1350 174.5599 0013427 271.3719 153.1038 16.32944071135764
| Epoch (UTC): | 06 April 2023 08:39:03 |
| Eccentricity: | 0.0013427 |
| inclination: | 97.1350° |
| perigee height: | 176 km |
| apogee height: | 193 km |
| right ascension of ascending node: | 174.5599° |
| argument of perigee: | 271.3719° |
| revolutions per day: | 16.32944071 |
| mean anomaly at epoch: | 153.1038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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