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 26160.28533870 +.00000000 +00000-0 -66117-4 0 00002
2 31792 70.9374 11.0694 0007215 150.1446 210.0088 14.12929724 01
| Epoch (UTC): | 09 June 2026 06:50:53 |
| Eccentricity: | 0.0007215 |
| inclination: | 70.9374° |
| perigee height: | 844 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 11.0694° |
| argument of perigee: | 150.1446° |
| revolutions per day: | 14.12929724 |
| mean anomaly at epoch: | 210.0088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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