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 54167C 22141L 23086.06854167 .00003835 00000-0 24051-3 0 860
2 54167 53.2144 175.9904 0001155 78.3306 353.2847 15.08832827 15
| Epoch (UTC): | 27 March 2023 01:38:42 |
| Eccentricity: | 0.0001155 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 175.9904° |
| argument of perigee: | 78.3306° |
| revolutions per day: | 15.08832827 |
| mean anomaly at epoch: | 353.2847° |
| 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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