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 22184.93154933 .00009787 00000-0 26758-3 0 9998
2 39026 97.2684 175.4667 0032494 99.5649 260.9270 15.37031262531519
| Epoch (UTC): | 03 July 2022 22:21:25 |
| Eccentricity: | 0.0032494 |
| inclination: | 97.2684° |
| perigee height: | 432 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 175.4667° |
| argument of perigee: | 99.5649° |
| revolutions per day: | 15.37031262 |
| mean anomaly at epoch: | 260.9270° |
| orbit number at epoch: | 53151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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