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 43077U 26145.24846308 +.00000000 +00000-0 +15772-4 0 00003
2 43077 86.3957 331.5852 0002235 90.2142 269.9309 14.34217743 02
| Epoch (UTC): | 25 May 2026 05:57:47 |
| Eccentricity: | 0.0002235 |
| inclination: | 86.3957° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 331.5852° |
| argument of perigee: | 90.2142° |
| revolutions per day: | 14.34217743 |
| mean anomaly at epoch: | 269.9309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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