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 46U 60007B 23030.25701941 .00000518 00000-0 12516-3 0 9992
2 46 66.6917 340.2305 0203106 139.1988 222.4534 14.50068793277770
| Epoch (UTC): | 30 January 2023 06:10:06 |
| Eccentricity: | 0.0203106 |
| inclination: | 66.6917° |
| perigee height: | 581 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 340.2305° |
| argument of perigee: | 139.1988° |
| revolutions per day: | 14.50068793 |
| mean anomaly at epoch: | 222.4534° |
| orbit number at epoch: | 27777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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