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 54194C 22141AP 24358.49493056 -.00011559 00000+0 -72487-3 0 3587
2 54194 53.2149 174.6795 0001351 86.3189 250.4627 15.08848848 14
| Epoch (UTC): | 23 December 2024 11:52:42 |
| Eccentricity: | 0.0001351 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 174.6795° |
| argument of perigee: | 86.3189° |
| revolutions per day: | 15.08848848 |
| mean anomaly at epoch: | 250.4627° |
| 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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