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 62732U 26145.57326072 +.00000000 +00000-0 +17696-3 0 00005
2 62732 97.6534 314.9690 0010107 106.1142 254.1201 15.11162513 03
| Epoch (UTC): | 25 May 2026 13:45:29 |
| Eccentricity: | 0.0010107 |
| inclination: | 97.6534° |
| perigee height: | 526 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 314.9690° |
| argument of perigee: | 106.1142° |
| revolutions per day: | 15.11162513 |
| mean anomaly at epoch: | 254.1201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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