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 2016U 66013A 23083.24115454 .00002811 00000-0 80638-3 0 9997
2 2016 34.0986 280.6292 1181879 275.7200 71.0137 12.61160893590558
| Epoch (UTC): | 24 March 2023 05:47:15 |
| Eccentricity: | 0.1181879 |
| inclination: | 34.0986° |
| perigee height: | 497 km |
| apogee height: | 2339 km |
| right ascension of ascending node: | 280.6292° |
| argument of perigee: | 275.7200° |
| revolutions per day: | 12.61160893 |
| mean anomaly at epoch: | 71.0137° |
| orbit number at epoch: | 59055 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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