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 00046U 60007B 22333.52374532 .00000820 00000-0 18234-3 0 9998
2 00046 66.6880 147.2192 0209549 185.7327 174.1383 14.49916205268839
| Epoch (UTC): | 29 November 2022 12:34:11 |
| Eccentricity: | 0.0209549 |
| inclination: | 66.6880° |
| perigee height: | 577 km |
| apogee height: | 875 km |
| right ascension of ascending node: | 147.2192° |
| argument of perigee: | 185.7327° |
| revolutions per day: | 14.49916205 |
| mean anomaly at epoch: | 174.1383° |
| orbit number at epoch: | 26883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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