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 24278.86225708 .00000659 00000-0 34800-3 0 9997
2 17974 71.0089 50.7981 0016139 279.3320 248.6349 14.17500493934276
| Epoch (UTC): | 04 October 2024 20:41:39 |
| Eccentricity: | 0.0016139 |
| inclination: | 71.0089° |
| perigee height: | 822 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 50.7981° |
| argument of perigee: | 279.3320° |
| revolutions per day: | 14.17500493 |
| mean anomaly at epoch: | 248.6349° |
| orbit number at epoch: | 93427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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