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 57876U 26145.45057922 +.00000000 +00000-0 +31936-4 0 00004
2 57876 43.0030 211.9905 0001573 273.0415 87.0257 15.27578101 06
| Epoch (UTC): | 25 May 2026 10:48:50 |
| Eccentricity: | 0.0001573 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.9905° |
| argument of perigee: | 273.0415° |
| revolutions per day: | 15.27578101 |
| mean anomaly at epoch: | 87.0257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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