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 43651U 26145.57046838 +.00000000 +00000-0 +00000-0 0 00001
2 43651 1.4286 2.0665 0062063 357.3125 21.5843 1.00268646 00
| Epoch (UTC): | 25 May 2026 13:41:28 |
| Eccentricity: | 0.0062063 |
| inclination: | 1.4286° |
| perigee height: | 35526 km |
| apogee height: | 36049 km |
| right ascension of ascending node: | 2.0665° |
| argument of perigee: | 357.3125° |
| revolutions per day: | 1.00268646 |
| mean anomaly at epoch: | 21.5843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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