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 59752U 26145.27090652 +.00000000 +00000-0 -47943-6 0 00004
2 59752 42.9997 110.8847 0000823 245.8131 114.2635 15.27564796 00
| Epoch (UTC): | 25 May 2026 06:30:06 |
| Eccentricity: | 0.0000823 |
| inclination: | 42.9997° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.8847° |
| argument of perigee: | 245.8131° |
| revolutions per day: | 15.27564796 |
| mean anomaly at epoch: | 114.2635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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