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 22178.40870035 .00000886 00000-0 14564-3 0 9999
2 39161 97.9072 255.3858 0010184 37.6369 322.5551 14.72971198490937
| Epoch (UTC): | 27 June 2022 09:48:31 |
| Eccentricity: | 0.0010184 |
| inclination: | 97.9072° |
| perigee height: | 644 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 255.3858° |
| argument of perigee: | 37.6369° |
| revolutions per day: | 14.72971198 |
| mean anomaly at epoch: | 322.5551° |
| orbit number at epoch: | 49093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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