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 22143.51275930 .00023936 00000-0 67469-3 0 9994
2 39026 97.2678 134.5338 0028738 246.5656 113.2566 15.35999533525154
| Epoch (UTC): | 23 May 2022 12:18:22 |
| Eccentricity: | 0.0028738 |
| inclination: | 97.2678° |
| perigee height: | 438 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 134.5338° |
| argument of perigee: | 246.5656° |
| revolutions per day: | 15.35999533 |
| mean anomaly at epoch: | 113.2566° |
| orbit number at epoch: | 52515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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