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 31792U 26145.41822363 +.00000000 +00000-0 -10540-3 0 00006
2 31792 70.9395 42.2829 0007596 178.0054 182.1099 14.12934596 00
| Epoch (UTC): | 25 May 2026 10:02:14 |
| Eccentricity: | 0.0007596 |
| inclination: | 70.9395° |
| perigee height: | 844 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 42.2829° |
| argument of perigee: | 178.0054° |
| revolutions per day: | 14.12934596 |
| mean anomaly at epoch: | 182.1099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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