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 56884U 26145.31513338 +.00000000 +00000-0 +18983-4 0 00002
2 56884 43.0039 12.0768 0001121 265.1225 94.9499 15.27580258 01
| Epoch (UTC): | 25 May 2026 07:33:47 |
| Eccentricity: | 0.0001121 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.0768° |
| argument of perigee: | 265.1225° |
| revolutions per day: | 15.27580258 |
| mean anomaly at epoch: | 94.9499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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