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 39482U 13075B 20244.00915009 .38339406 -15773-4 34065-3 0 9993
2 39482 23.8923 11.2118 0142891 173.5806 332.1179 16.27115612107662
| Epoch (UTC): | 31 August 2020 00:13:10 |
| Eccentricity: | 0.0142891 |
| inclination: | 23.8923° |
| perigee height: | 106 km |
| apogee height: | 294 km |
| right ascension of ascending node: | 11.2118° |
| argument of perigee: | 173.5806° |
| revolutions per day: | 16.27115612 |
| mean anomaly at epoch: | 332.1179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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