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 23081.51958726 .00016081 00000-0 11543-2 0 9992
2 33493 98.2488 90.0809 0015969 342.8572 17.2110 15.04306176770717
| Epoch (UTC): | 22 March 2023 12:28:12 |
| Eccentricity: | 0.0015969 |
| inclination: | 98.2488° |
| perigee height: | 542 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 90.0809° |
| argument of perigee: | 342.8572° |
| revolutions per day: | 15.04306176 |
| mean anomaly at epoch: | 17.2110° |
| orbit number at epoch: | 77071 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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