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 54182C 22141AB 23086.06715278 -.00020752 00000-0 -13605-2 0 867
2 54182 53.2175 135.6930 0001166 80.3067 199.7456 15.07227513 15
| Epoch (UTC): | 27 March 2023 01:36:42 |
| Eccentricity: | 0.0001166 |
| inclination: | 53.2175° |
| perigee height: | 544 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 135.6930° |
| argument of perigee: | 80.3067° |
| revolutions per day: | 15.07227513 |
| mean anomaly at epoch: | 199.7456° |
| 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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