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 55149U 23004K 24358.20274903 .00000118 00000-0 26773-3 0 9990
2 55149 87.9110 83.1475 0002434 111.3553 248.7839 13.18685396 98392
| Epoch (UTC): | 23 December 2024 04:51:57 |
| Eccentricity: | 0.0002434 |
| inclination: | 87.9110° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 83.1475° |
| argument of perigee: | 111.3553° |
| revolutions per day: | 13.18685396 |
| mean anomaly at epoch: | 248.7839° |
| orbit number at epoch: | 9839 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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