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 43463U 26145.25083902 +.00000000 +00000-0 +00000-0 0 00000
2 43463 0.0472 112.5841 0001949 310.2277 29.4357 1.00271699 07
| Epoch (UTC): | 25 May 2026 06:01:12 |
| Eccentricity: | 0.0001949 |
| inclination: | 0.0472° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 112.5841° |
| argument of perigee: | 310.2277° |
| revolutions per day: | 1.00271699 |
| mean anomaly at epoch: | 29.4357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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