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 05552U 71086F 24357.88419949 .00000002 00000-0 12975-3 0 9991
2 05552 74.0256 159.1256 0036876 52.7700 101.1905 12.38723421405451
| Epoch (UTC): | 22 December 2024 21:13:14 |
| Eccentricity: | 0.0036876 |
| inclination: | 74.0256° |
| perigee height: | 1483 km |
| apogee height: | 1541 km |
| right ascension of ascending node: | 159.1256° |
| argument of perigee: | 52.7700° |
| revolutions per day: | 12.38723421 |
| mean anomaly at epoch: | 101.1905° |
| orbit number at epoch: | 40545 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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