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 39439U 13066Z 22137.19027931 .00004875 00000-0 57132-3 0 9996
2 39439 97.6357 112.3676 0064305 141.4352 219.1483 14.83941591458506
| Epoch (UTC): | 17 May 2022 04:34:00 |
| Eccentricity: | 0.0064305 |
| inclination: | 97.6357° |
| perigee height: | 572 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 112.3676° |
| argument of perigee: | 141.4352° |
| revolutions per day: | 14.83941591 |
| mean anomaly at epoch: | 219.1483° |
| orbit number at epoch: | 45850 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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