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 56832U 26145.33866346 +.00000000 +00000-0 -11149-3 0 00004
2 56832 43.0047 8.3631 0001252 273.6401 86.4308 15.27599759 06
| Epoch (UTC): | 25 May 2026 08:07:40 |
| Eccentricity: | 0.0001252 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.3631° |
| argument of perigee: | 273.6401° |
| revolutions per day: | 15.27599759 |
| mean anomaly at epoch: | 86.4308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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