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 54184C 22141AD 23089.72895833 .00034441 00000-0 21592-2 0 896
2 54184 53.2155 149.4255 0001487 73.3100 172.1478 15.08812392 19
| Epoch (UTC): | 30 March 2023 17:29:42 |
| Eccentricity: | 0.0001487 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 149.4255° |
| argument of perigee: | 73.3100° |
| revolutions per day: | 15.08812392 |
| mean anomaly at epoch: | 172.1478° |
| 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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