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 56185U 26145.35320000 +.00000000 +00000-0 +45963-3 0 00009
2 56185 97.2958 62.0721 0007816 115.6814 244.5265 15.85782731 08
| Epoch (UTC): | 25 May 2026 08:28:36 |
| Eccentricity: | 0.0007816 |
| inclination: | 97.2958° |
| perigee height: | 309 km |
| apogee height: | 319 km |
| right ascension of ascending node: | 62.0721° |
| argument of perigee: | 115.6814° |
| revolutions per day: | 15.85782731 |
| mean anomaly at epoch: | 244.5265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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