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 22179.15594233 .00000835 00000-0 13760-3 0 9996
2 39161 97.9077 256.1137 0010197 35.3478 324.8407 14.72971975491042
| Epoch (UTC): | 28 June 2022 03:44:33 |
| Eccentricity: | 0.0010197 |
| inclination: | 97.9077° |
| perigee height: | 644 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 256.1137° |
| argument of perigee: | 35.3478° |
| revolutions per day: | 14.72971975 |
| mean anomaly at epoch: | 324.8407° |
| orbit number at epoch: | 49104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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