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 43824U 26145.52709845 +.00000000 +00000-0 +00000-0 0 00002
2 43824 0.0798 260.7515 0007716 179.8328 66.2812 1.00271868 00
| Epoch (UTC): | 25 May 2026 12:39:01 |
| Eccentricity: | 0.0007716 |
| inclination: | 0.0798° |
| perigee height: | 35754 km |
| apogee height: | 35819 km |
| right ascension of ascending node: | 260.7515° |
| argument of perigee: | 179.8328° |
| revolutions per day: | 1.00271868 |
| mean anomaly at epoch: | 66.2812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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