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 is defined by the following mean orbital elements,
1 43019U 98067NG 21342.21300676 .13504394 12696-4 19709-3 0 9990
2 43019 51.6308 29.9256 0003489 341.0244 128.1167 16.48645518317844
| Epoch (UTC): | 08 December 2021 05:06:43 |
| Eccentricity: | 0.0003489 |
| inclination: | 51.6308° |
| perigee height: | 140 km |
| apogee height: | 145 km |
| right ascension of ascending node: | 29.9256° |
| argument of perigee: | 341.0244° |
| revolutions per day: | 16.48645518 |
| mean anomaly at epoch: | 128.1167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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