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 32781U 26032.17115000 +.00000000 +00000-0 +00000-0 0 00002
2 32781 59.8823 41.1862 0005528 277.9152 82.0594 1.65404902 02
| Epoch (UTC): | 01 February 2026 04:06:27 |
| Eccentricity: | 0.0005528 |
| inclination: | 59.8823° |
| perigee height: | 23807 km |
| apogee height: | 23841 km |
| right ascension of ascending node: | 41.1862° |
| argument of perigee: | 277.9152° |
| revolutions per day: | 1.65404902 |
| mean anomaly at epoch: | 82.0594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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