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 17641U 81053LL 24280.12052909 .00021178 00000-0 10403-1 0 9998
2 17641 82.7537 56.4569 0052220 89.2164 85.2441 14.16840491 24007
| Epoch (UTC): | 06 October 2024 02:53:33 |
| Eccentricity: | 0.0052220 |
| inclination: | 82.7537° |
| perigee height: | 798 km |
| apogee height: | 874 km |
| right ascension of ascending node: | 56.4569° |
| argument of perigee: | 89.2164° |
| revolutions per day: | 14.16840491 |
| mean anomaly at epoch: | 85.2441° |
| orbit number at epoch: | 2400 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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