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 27431U 02024B 21023.81416909 .00000016 00000-0 35214-4 0 9997
2 27431 99.1480 31.4208 0015556 8.0812 352.0605 14.09713937961909
| Epoch (UTC): | 23 January 2021 19:32:24 |
| Eccentricity: | 0.0015556 |
| inclination: | 99.1480° |
| perigee height: | 849 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 31.4208° |
| argument of perigee: | 8.0812° |
| revolutions per day: | 14.09713937 |
| mean anomaly at epoch: | 352.0605° |
| orbit number at epoch: | 96190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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