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 57635U 26144.99639147 +.00000000 +00000-0 +19418-3 0 00000
2 57635 43.0035 21.8580 0001527 273.9507 86.1170 15.27567040 05
| Epoch (UTC): | 24 May 2026 23:54:48 |
| Eccentricity: | 0.0001527 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.8580° |
| argument of perigee: | 273.9507° |
| revolutions per day: | 15.27567040 |
| mean anomaly at epoch: | 86.1170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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