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 39679U 14021B 22143.53193565 .00003962 00000-0 19921-3 0 9996
2 39679 51.6154 72.0057 0164809 231.5261 127.0828 15.08567319445351
| Epoch (UTC): | 23 May 2022 12:45:59 |
| Eccentricity: | 0.0164809 |
| inclination: | 51.6154° |
| perigee height: | 426 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 72.0057° |
| argument of perigee: | 231.5261° |
| revolutions per day: | 15.08567319 |
| mean anomaly at epoch: | 127.0828° |
| orbit number at epoch: | 44535 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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