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 43130U 18004V 24056.51206482 .08342929 24643-5 76486-3 0 9994
2 43130 97.2783 149.1803 0010598 269.1581 90.8504 16.38778103341851
| Epoch (UTC): | 25 February 2024 12:17:22 |
| Eccentricity: | 0.0010598 |
| inclination: | 97.2783° |
| perigee height: | 162 km |
| apogee height: | 176 km |
| right ascension of ascending node: | 149.1803° |
| argument of perigee: | 269.1581° |
| revolutions per day: | 16.38778103 |
| mean anomaly at epoch: | 90.8504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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