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 26039.74547470 +.00000000 +00000-0 +19734-3 0 00001
2 32792 98.1425 38.4193 0025278 34.9515 325.3353 14.86006118 02
| Epoch (UTC): | 08 February 2026 17:53:29 |
| Eccentricity: | 0.0025278 |
| inclination: | 98.1425° |
| perigee height: | 593 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 38.4193° |
| argument of perigee: | 34.9515° |
| revolutions per day: | 14.86006118 |
| mean anomaly at epoch: | 325.3353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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