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 31879U 99025CKE 22221.10949155 .00000244 00000-0 78694-4 0 9994
2 31879 99.7137 280.0738 0225376 321.1329 37.3830 14.37003182456323
| Epoch (UTC): | 09 August 2022 02:37:40 |
| Eccentricity: | 0.0225376 |
| inclination: | 99.7137° |
| perigee height: | 607 km |
| apogee height: | 929 km |
| right ascension of ascending node: | 280.0738° |
| argument of perigee: | 321.1329° |
| revolutions per day: | 14.37003182 |
| mean anomaly at epoch: | 37.3830° |
| orbit number at epoch: | 45632 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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