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 63326U 26145.47583316 +.00000000 +00000-0 +56105-3 0 00008
2 63326 43.0000 316.9461 0001519 251.4400 108.6286 15.27599365 04
| Epoch (UTC): | 25 May 2026 11:25:11 |
| Eccentricity: | 0.0001519 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.9461° |
| argument of perigee: | 251.4400° |
| revolutions per day: | 15.27599365 |
| mean anomaly at epoch: | 108.6286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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