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 33493U 09002B 23336.79869087 .00016609 00000-0 99163-3 0 9997
2 33493 98.2333 3.5972 0013877 193.5519 166.5339 15.11125089809178
| Epoch (UTC): | 02 December 2023 19:10:06 |
| Eccentricity: | 0.0013877 |
| inclination: | 98.2333° |
| perigee height: | 523 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 3.5972° |
| argument of perigee: | 193.5519° |
| revolutions per day: | 15.11125089 |
| mean anomaly at epoch: | 166.5339° |
| orbit number at epoch: | 80917 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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