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 42983U 98067NF 22207.34139113 .10906988 12776-4 92768-4 0 9998
2 42983 51.6099 330.8193 0006097 301.9164 58.1274 16.51583326271200
| Epoch (UTC): | 26 July 2022 08:11:36 |
| Eccentricity: | 0.0006097 |
| inclination: | 51.6099° |
| perigee height: | 131 km |
| apogee height: | 139 km |
| right ascension of ascending node: | 330.8193° |
| argument of perigee: | 301.9164° |
| revolutions per day: | 16.51583326 |
| mean anomaly at epoch: | 58.1274° |
| orbit number at epoch: | 27120 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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