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 00016U 58002A 22147.62511477 -.00000004 00000-0 17289-6 0 9999
2 00016 34.2661 266.8935 2025777 348.0251 7.8334 10.48823334533296
| Epoch (UTC): | 27 May 2022 15:00:09 |
| Eccentricity: | 0.2025777 |
| inclination: | 34.2661° |
| perigee height: | 652 km |
| apogee height: | 4223 km |
| right ascension of ascending node: | 266.8935° |
| argument of perigee: | 348.0251° |
| revolutions per day: | 10.48823334 |
| mean anomaly at epoch: | 7.8334° |
| orbit number at epoch: | 53329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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