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 55006U 22151UW 24277.27977468 .00007542 00000-0 40745-2 0 9999
2 55006 98.8116 278.1451 0042965 299.0460 60.6411 14.12400163 96213
| Epoch (UTC): | 03 October 2024 06:42:52 |
| Eccentricity: | 0.0042965 |
| inclination: | 98.8116° |
| perigee height: | 820 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 278.1451° |
| argument of perigee: | 299.0460° |
| revolutions per day: | 14.12400163 |
| mean anomaly at epoch: | 60.6411° |
| orbit number at epoch: | 9621 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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