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 24262.23727759 .00004183 00000-0 81628-3 0 9995
2 00046 66.6907 162.3427 0194747 50.0821 311.7222 14.52586756364403
| Epoch (UTC): | 18 September 2024 05:41:40 |
| Eccentricity: | 0.0194747 |
| inclination: | 66.6907° |
| perigee height: | 579 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 162.3427° |
| argument of perigee: | 50.0821° |
| revolutions per day: | 14.52586756 |
| mean anomaly at epoch: | 311.7222° |
| orbit number at epoch: | 36440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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