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 32790U 26145.35839183 +.00000000 +00000-0 +29690-3 0 00001
2 32790 97.8624 124.6976 0011666 117.7152 242.5259 15.05422019 06
| Epoch (UTC): | 25 May 2026 08:36:05 |
| Eccentricity: | 0.0011666 |
| inclination: | 97.8624° |
| perigee height: | 542 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 124.6976° |
| argument of perigee: | 117.7152° |
| revolutions per day: | 15.05422019 |
| mean anomaly at epoch: | 242.5259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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