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 59734U 26145.34753784 +.00000000 +00000-0 +35764-4 0 00009
2 59734 43.0032 103.6787 0001244 259.4774 100.5937 15.27579268 00
| Epoch (UTC): | 25 May 2026 08:20:27 |
| Eccentricity: | 0.0001244 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.6787° |
| argument of perigee: | 259.4774° |
| revolutions per day: | 15.27579268 |
| mean anomaly at epoch: | 100.5937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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