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 26162.26762414 +.00000000 +00000-0 -55969-4 0 00003
2 31792 70.9372 6.9071 0007226 146.3925 213.7656 14.12929247 03
| Epoch (UTC): | 11 June 2026 06:25:22 |
| Eccentricity: | 0.0007226 |
| inclination: | 70.9372° |
| perigee height: | 844 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 6.9071° |
| argument of perigee: | 146.3925° |
| revolutions per day: | 14.12929247 |
| mean anomaly at epoch: | 213.7656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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