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 57707U 26144.99262788 +.00000000 +00000-0 +24682-2 0 00001
2 57707 42.9986 11.9871 0026635 225.0742 134.7951 15.34846309 00
| Epoch (UTC): | 24 May 2026 23:49:23 |
| Eccentricity: | 0.0026635 |
| inclination: | 42.9986° |
| perigee height: | 443 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 11.9871° |
| argument of perigee: | 225.0742° |
| revolutions per day: | 15.34846309 |
| mean anomaly at epoch: | 134.7951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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