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 43786U 26156.36171225 +.00000000 +00000-0 +35770-3 0 00003
2 43786 97.4030 208.1104 0013338 40.5492 319.6733 15.18900130 01
| Epoch (UTC): | 05 June 2026 08:40:51 |
| Eccentricity: | 0.0013338 |
| inclination: | 97.4030° |
| perigee height: | 500 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 208.1104° |
| argument of perigee: | 40.5492° |
| revolutions per day: | 15.18900130 |
| mean anomaly at epoch: | 319.6733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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