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 32785U 26135.23222227 +.00000000 +00000-0 +21474-3 0 00008
2 32785 97.8261 115.9779 0010154 133.5668 226.6405 15.09118471 04
| Epoch (UTC): | 15 May 2026 05:34:24 |
| Eccentricity: | 0.0010154 |
| inclination: | 97.8261° |
| perigee height: | 532 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 115.9779° |
| argument of perigee: | 133.5668° |
| revolutions per day: | 15.09118471 |
| mean anomaly at epoch: | 226.6405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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