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 43867U 26144.74208219 +.00000000 +00000-0 +00000-0 0 00001
2 43867 0.0453 109.6388 0000252 46.5591 63.2876 1.00277164 06
| Epoch (UTC): | 24 May 2026 17:48:35 |
| Eccentricity: | 0.0000252 |
| inclination: | 0.0453° |
| perigee height: | 35784 km |
| apogee height: | 35786 km |
| right ascension of ascending node: | 109.6388° |
| argument of perigee: | 46.5591° |
| revolutions per day: | 1.00277164 |
| mean anomaly at epoch: | 63.2876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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