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 22178.74835536 .00000859 00000-0 14131-3 0 9993
2 39161 97.9077 255.7167 0010221 36.4564 323.7308 14.72971511490982
| Epoch (UTC): | 27 June 2022 17:57:37 |
| Eccentricity: | 0.0010221 |
| inclination: | 97.9077° |
| perigee height: | 644 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 255.7167° |
| argument of perigee: | 36.4564° |
| revolutions per day: | 14.72971511 |
| mean anomaly at epoch: | 323.7308° |
| orbit number at epoch: | 49098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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