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 31850U 99025CJQ 23335.15352114 .00037526 00000-0 46728-2 0 9992
2 31850 98.5888 301.2025 0234359 340.2725 18.9523 14.64824571547597
| Epoch (UTC): | 01 December 2023 03:41:04 |
| Eccentricity: | 0.0234359 |
| inclination: | 98.5888° |
| perigee height: | 512 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 301.2025° |
| argument of perigee: | 340.2725° |
| revolutions per day: | 14.64824571 |
| mean anomaly at epoch: | 18.9523° |
| orbit number at epoch: | 54759 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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