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 54174C 22141T 23089.72131944 -.00962642 00000-0 -74354-2 0 890
2 54174 53.2140 102.6235 0000832 82.7908 325.4013 15.72218142 16
| Epoch (UTC): | 30 March 2023 17:18:42 |
| Eccentricity: | 0.0000832 |
| inclination: | 53.2140° |
| perigee height: | 352 km |
| apogee height: | 353 km |
| right ascension of ascending node: | 102.6235° |
| argument of perigee: | 82.7908° |
| revolutions per day: | 15.72218142 |
| mean anomaly at epoch: | 325.4013° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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