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 23038.25778323 .00001020 00000-0 22423-3 0 9995
2 00046 66.6916 318.5882 0202517 133.0661 228.7604 14.50083483278943
| Epoch (UTC): | 07 February 2023 06:11:12 |
| Eccentricity: | 0.0202517 |
| inclination: | 66.6916° |
| perigee height: | 581 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 318.5882° |
| argument of perigee: | 133.0661° |
| revolutions per day: | 14.50083483 |
| mean anomaly at epoch: | 228.7604° |
| orbit number at epoch: | 27894 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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