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 23029.22243280 .00000586 00000-0 13840-3 0 9990
2 00046 66.6917 343.0291 0203193 139.9909 221.6374 14.50067532277630
| Epoch (UTC): | 29 January 2023 05:20:18 |
| Eccentricity: | 0.0203193 |
| inclination: | 66.6917° |
| perigee height: | 581 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 343.0291° |
| argument of perigee: | 139.9909° |
| revolutions per day: | 14.50067532 |
| mean anomaly at epoch: | 221.6374° |
| orbit number at epoch: | 27763 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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