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 43920U 26145.53817933 +.00000000 +00000-0 +00000-0 0 00008
2 43920 0.0134 311.5905 0000943 43.7311 211.5283 1.00267852 00
| Epoch (UTC): | 25 May 2026 12:54:58 |
| Eccentricity: | 0.0000943 |
| inclination: | 0.0134° |
| perigee height: | 35784 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 311.5905° |
| argument of perigee: | 43.7311° |
| revolutions per day: | 1.00267852 |
| mean anomaly at epoch: | 211.5283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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