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 57930U 26145.66668980 +.00000000 +00000-0 +37873-3 0 00005
2 57930 42.9927 183.4966 0016787 224.3286 260.6736 15.73424550 08
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0016787 |
| inclination: | 42.9927° |
| perigee height: | 338 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 183.4966° |
| argument of perigee: | 224.3286° |
| revolutions per day: | 15.73424550 |
| mean anomaly at epoch: | 260.6736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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