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 17974U 87041B 24284.56098704 .00000198 00000-0 12116-3 0 9999
2 17974 71.0101 38.7865 0016231 271.9519 167.9946 14.17504838935329
| Epoch (UTC): | 10 October 2024 13:27:49 |
| Eccentricity: | 0.0016231 |
| inclination: | 71.0101° |
| perigee height: | 822 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 38.7865° |
| argument of perigee: | 271.9519° |
| revolutions per day: | 14.17504838 |
| mean anomaly at epoch: | 167.9946° |
| orbit number at epoch: | 93532 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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