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 39439U 13066Z 22179.86766270 .00002423 00000-0 28531-3 0 9990
2 39439 97.6369 153.2325 0062999 4.2855 355.8886 14.84290448463741
| Epoch (UTC): | 28 June 2022 20:49:26 |
| Eccentricity: | 0.0062999 |
| inclination: | 97.6369° |
| perigee height: | 572 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 153.2325° |
| argument of perigee: | 4.2855° |
| revolutions per day: | 14.84290448 |
| mean anomaly at epoch: | 355.8886° |
| orbit number at epoch: | 46374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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