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 66013U 26145.62271705 +.00000000 +00000-0 +49249-3 0 00008
2 66013 53.1598 106.6130 0000731 120.1055 240.0019 15.30209417 09
| Epoch (UTC): | 25 May 2026 14:56:42 |
| Eccentricity: | 0.0000731 |
| inclination: | 53.1598° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.6130° |
| argument of perigee: | 120.1055° |
| revolutions per day: | 15.30209417 |
| mean anomaly at epoch: | 240.0019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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