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 32791U 26038.93577524 +.00000000 +00000-0 +80657-3 0 00005
2 32791 97.7495 31.1687 0005273 65.8712 294.3077 15.27753388 08
| Epoch (UTC): | 07 February 2026 22:27:30 |
| Eccentricity: | 0.0005273 |
| inclination: | 97.7495° |
| perigee height: | 479 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 31.1687° |
| argument of perigee: | 65.8712° |
| revolutions per day: | 15.27753388 |
| mean anomaly at epoch: | 294.3077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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