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 33933U 93036EN 23345.01095050 .00000615 00000-0 23650-3 0 9990
2 33933 74.0897 312.9046 0074417 151.5901 208.9339 14.30870108772998
| Epoch (UTC): | 11 December 2023 00:15:46 |
| Eccentricity: | 0.0074417 |
| inclination: | 74.0897° |
| perigee height: | 735 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 312.9046° |
| argument of perigee: | 151.5901° |
| revolutions per day: | 14.30870108 |
| mean anomaly at epoch: | 208.9339° |
| orbit number at epoch: | 77299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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