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 23789U 96009C 23084.13038316 .00000054 00000-0 23988-3 0 9997
2 23789 82.5843 353.2646 0004341 210.2756 149.8085 12.62632864248778
| Epoch (UTC): | 25 March 2023 03:07:45 |
| Eccentricity: | 0.0004341 |
| inclination: | 82.5843° |
| perigee height: | 1409 km |
| apogee height: | 1415 km |
| right ascension of ascending node: | 353.2646° |
| argument of perigee: | 210.2756° |
| revolutions per day: | 12.62632864 |
| mean anomaly at epoch: | 149.8085° |
| orbit number at epoch: | 24877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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