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 17291U 87001B 24280.62533914 .00000129 00000-0 10198-3 0 9999
2 17291 82.4666 237.5939 0012407 119.5803 240.6595 13.84649754907685
| Epoch (UTC): | 06 October 2024 15:00:29 |
| Eccentricity: | 0.0012407 |
| inclination: | 82.4666° |
| perigee height: | 938 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 237.5939° |
| argument of perigee: | 119.5803° |
| revolutions per day: | 13.84649754 |
| mean anomaly at epoch: | 240.6595° |
| orbit number at epoch: | 90768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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