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 43468U 98067NR 20064.05831928 .04860327 12102-4 10158-2 0 9990
2 43468 51.6208 66.1430 0002240 149.8670 210.2481 16.30203714203978
| Epoch (UTC): | 04 March 2020 01:23:58 |
| Eccentricity: | 0.0002240 |
| inclination: | 51.6208° |
| perigee height: | 190 km |
| apogee height: | 193 km |
| right ascension of ascending node: | 66.1430° |
| argument of perigee: | 149.8670° |
| revolutions per day: | 16.30203714 |
| mean anomaly at epoch: | 210.2481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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