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 23404U 94077A 23153.03844668 -.00000012 00000-0 18702-4 0 9999
2 23404 71.0168 57.8927 0013305 81.8507 278.4124 14.13643933471543
| Epoch (UTC): | 02 June 2023 00:55:21 |
| Eccentricity: | 0.0013305 |
| inclination: | 71.0168° |
| perigee height: | 837 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 57.8927° |
| argument of perigee: | 81.8507° |
| revolutions per day: | 14.13643933 |
| mean anomaly at epoch: | 278.4124° |
| orbit number at epoch: | 47154 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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