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 24276.90235101 .00005788 00000-0 11158-2 0 9991
2 46 66.6887 122.5086 0195558 38.8203 322.6768 14.52691306366527
| Epoch (UTC): | 02 October 2024 21:39:23 |
| Eccentricity: | 0.0195558 |
| inclination: | 66.6887° |
| perigee height: | 578 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 122.5086° |
| argument of perigee: | 38.8203° |
| revolutions per day: | 14.52691306 |
| mean anomaly at epoch: | 322.6768° |
| orbit number at epoch: | 36652 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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