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 39161U 13021C 22179.76732120 .00000810 00000-0 13381-3 0 9994
2 39161 97.9071 256.7093 0010213 33.2756 326.9079 14.72972766491135
| Epoch (UTC): | 28 June 2022 18:24:56 |
| Eccentricity: | 0.0010213 |
| inclination: | 97.9071° |
| perigee height: | 644 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 256.7093° |
| argument of perigee: | 33.2756° |
| revolutions per day: | 14.72972766 |
| mean anomaly at epoch: | 326.9079° |
| orbit number at epoch: | 49113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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