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 54177C 22141W 23084.72270833 .00058824 00000-0 36865-2 0 845
2 54177 53.2154 172.2128 0001228 128.5631 108.5843 15.08801089 18
| Epoch (UTC): | 25 March 2023 17:20:42 |
| Eccentricity: | 0.0001228 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 172.2128° |
| argument of perigee: | 128.5631° |
| revolutions per day: | 15.08801089 |
| mean anomaly at epoch: | 108.5843° |
| 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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