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 48715U 02032AY 23027.32380945 .00008729 00000-0 35482-2 0 9990
2 48715 98.7092 337.5449 0035158 296.1736 63.5830 14.27440622 93787
| Epoch (UTC): | 27 January 2023 07:46:17 |
| Eccentricity: | 0.0035158 |
| inclination: | 98.7092° |
| perigee height: | 775 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 337.5449° |
| argument of perigee: | 296.1736° |
| revolutions per day: | 14.27440622 |
| mean anomaly at epoch: | 63.5830° |
| orbit number at epoch: | 9378 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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