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 57127U 26145.44710251 +.00000000 +00000-0 +45833-4 0 00004
2 57127 43.0024 207.8697 0001584 273.6761 86.3910 15.27584374 09
| Epoch (UTC): | 25 May 2026 10:43:49 |
| Eccentricity: | 0.0001584 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.8697° |
| argument of perigee: | 273.6761° |
| revolutions per day: | 15.27584374 |
| mean anomaly at epoch: | 86.3910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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