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 39026U 12072A 22181.48101749 .00007122 00000-0 19581-3 0 9999
2 39026 97.2676 172.0542 0032466 111.1332 249.3388 15.36965480530982
| Epoch (UTC): | 30 June 2022 11:32:39 |
| Eccentricity: | 0.0032466 |
| inclination: | 97.2676° |
| perigee height: | 433 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 172.0542° |
| argument of perigee: | 111.1332° |
| revolutions per day: | 15.36965480 |
| mean anomaly at epoch: | 249.3388° |
| orbit number at epoch: | 53098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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