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 43633U 26145.26071905 +.00000000 +00000-0 +00000-0 0 00000
2 43633 0.0063 71.0113 0000764 207.4134 227.2697 1.00272733 01
| Epoch (UTC): | 25 May 2026 06:15:26 |
| Eccentricity: | 0.0000764 |
| inclination: | 0.0063° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 71.0113° |
| argument of perigee: | 207.4134° |
| revolutions per day: | 1.00272733 |
| mean anomaly at epoch: | 227.2697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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