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 43999U 26059.23266965 +.00000000 +00000-0 +00000-0 0 00008
2 43999 19.7943 160.8102 4758962 136.0835 273.3883 1.85336317 05
| Epoch (UTC): | 28 February 2026 05:35:02 |
| Eccentricity: | 0.4758962 |
| inclination: | 19.7943° |
| perigee height: | 8295 km |
| apogee height: | 34941 km |
| right ascension of ascending node: | 160.8102° |
| argument of perigee: | 136.0835° |
| revolutions per day: | 1.85336317 |
| mean anomaly at epoch: | 273.3883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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