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 24276.81497226 .00000627 00000-0 33241-3 0 9999
2 17974 71.0082 55.1135 0016075 282.0871 241.7229 14.17497966933988
| Epoch (UTC): | 02 October 2024 19:33:33 |
| Eccentricity: | 0.0016075 |
| inclination: | 71.0082° |
| perigee height: | 822 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 55.1135° |
| argument of perigee: | 282.0871° |
| revolutions per day: | 14.17497966 |
| mean anomaly at epoch: | 241.7229° |
| orbit number at epoch: | 93398 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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