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 54157C 22141A 23084.72340278 .00057072 00000-0 35744-2 0 843
2 54157 53.2154 182.3358 0001079 75.6302 90.2371 15.08827374 12
| Epoch (UTC): | 25 March 2023 17:21:42 |
| Eccentricity: | 0.0001079 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 182.3358° |
| argument of perigee: | 75.6302° |
| revolutions per day: | 15.08827374 |
| mean anomaly at epoch: | 90.2371° |
| 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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