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 59740U 26145.36969543 +.00000000 +00000-0 +66503-4 0 00005
2 59740 43.0025 110.7622 0001107 251.3148 108.7583 15.27583344 07
| Epoch (UTC): | 25 May 2026 08:52:21 |
| Eccentricity: | 0.0001107 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.7622° |
| argument of perigee: | 251.3148° |
| revolutions per day: | 15.27583344 |
| mean anomaly at epoch: | 108.7583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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