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 is defined by the following mean orbital elements,
1 43567U 26143.50341516 +.00000000 +00000-0 +00000-0 0 00009
2 43567 57.1794 342.4508 0002695 325.3655 34.6368 1.70475670 04
| Epoch (UTC): | 23 May 2026 12:04:55 |
| Eccentricity: | 0.0002695 |
| inclination: | 57.1794° |
| perigee height: | 23214 km |
| apogee height: | 23230 km |
| right ascension of ascending node: | 342.4508° |
| argument of perigee: | 325.3655° |
| revolutions per day: | 1.70475670 |
| mean anomaly at epoch: | 34.6368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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