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 22147.90406811 .00001810 00000-0 10061-3 0 9998
2 39679 51.6167 51.6502 0164636 246.7677 111.5884 15.08591308446019
| Epoch (UTC): | 27 May 2022 21:41:51 |
| Eccentricity: | 0.0164636 |
| inclination: | 51.6167° |
| perigee height: | 426 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 51.6502° |
| argument of perigee: | 246.7677° |
| revolutions per day: | 15.08591308 |
| mean anomaly at epoch: | 111.5884° |
| orbit number at epoch: | 44601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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