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 23337.06766505 .00001865 00000-0 37210-3 0 9992
2 46 66.6901 229.4904 0212180 268.4659 89.2137 14.51157816322279
| Epoch (UTC): | 03 December 2023 01:37:26 |
| Eccentricity: | 0.0212180 |
| inclination: | 66.6901° |
| perigee height: | 571 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 229.4904° |
| argument of perigee: | 268.4659° |
| revolutions per day: | 14.51157816 |
| mean anomaly at epoch: | 89.2137° |
| orbit number at epoch: | 32227 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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