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 23150.04157194 .00001122 00000-0 24275-3 0 9994
2 00046 66.6912 16.0748 0201169 46.7111 315.0580 14.50542572295156
| Epoch (UTC): | 30 May 2023 00:59:51 |
| Eccentricity: | 0.0201169 |
| inclination: | 66.6912° |
| perigee height: | 581 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 16.0748° |
| argument of perigee: | 46.7111° |
| revolutions per day: | 14.50542572 |
| mean anomaly at epoch: | 315.0580° |
| orbit number at epoch: | 29515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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