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 56836U 26145.04376191 +.00000000 +00000-0 +83173-4 0 00006
2 56836 43.0002 32.6004 0001147 273.2761 86.7959 15.27586829 02
| Epoch (UTC): | 25 May 2026 01:03:01 |
| Eccentricity: | 0.0001147 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 32.6004° |
| argument of perigee: | 273.2761° |
| revolutions per day: | 15.27586829 |
| mean anomaly at epoch: | 86.7959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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