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 57871U 26145.50440029 +.00000000 +00000-0 +52525-3 0 00005
2 57871 43.0037 211.5325 0001436 273.5727 86.4960 15.27589296 00
| Epoch (UTC): | 25 May 2026 12:06:20 |
| Eccentricity: | 0.0001436 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.5325° |
| argument of perigee: | 273.5727° |
| revolutions per day: | 15.27589296 |
| mean anomaly at epoch: | 86.4960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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