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 17369U 87011A 24284.39450804 .00000298 00000-0 14845-3 0 9990
2 17369 65.0109 169.9221 0021051 260.9536 98.9166 14.31712963 20771
| Epoch (UTC): | 10 October 2024 09:28:05 |
| Eccentricity: | 0.0021051 |
| inclination: | 65.0109° |
| perigee height: | 771 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 169.9221° |
| argument of perigee: | 260.9536° |
| revolutions per day: | 14.31712963 |
| mean anomaly at epoch: | 98.9166° |
| orbit number at epoch: | 2077 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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