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 33892U 93036CV 23340.47996205 .00001491 00000-0 67467-3 0 9998
2 33892 73.8064 2.5257 0120282 165.8811 324.3004 14.19123959764806
| Epoch (UTC): | 06 December 2023 11:31:08 |
| Eccentricity: | 0.0120282 |
| inclination: | 73.8064° |
| perigee height: | 741 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 2.5257° |
| argument of perigee: | 165.8811° |
| revolutions per day: | 14.19123959 |
| mean anomaly at epoch: | 324.3004° |
| orbit number at epoch: | 76480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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