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 32792U 26155.07866213 +.00000000 +00000-0 +14366-3 0 00001
2 32792 98.1447 156.5229 0024735 19.9903 340.2275 14.86294868 09
| Epoch (UTC): | 04 June 2026 01:53:16 |
| Eccentricity: | 0.0024735 |
| inclination: | 98.1447° |
| perigee height: | 592 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 156.5229° |
| argument of perigee: | 19.9903° |
| revolutions per day: | 14.86294868 |
| mean anomaly at epoch: | 340.2275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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