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 15332U 26044.68054338 +.00000000 +00000-0 +51745-4 0 00006
2 15332 82.5329 108.1275 0020298 13.0584 104.5029 14.85814561 05
| Epoch (UTC): | 13 February 2026 16:19:58 |
| Eccentricity: | 0.0020298 |
| inclination: | 82.5329° |
| perigee height: | 597 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 108.1275° |
| argument of perigee: | 13.0584° |
| revolutions per day: | 14.85814561 |
| mean anomaly at epoch: | 104.5029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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