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 59749U 26145.36584109 +.00000000 +00000-0 -24334-4 0 00002
2 59749 43.0032 110.7324 0001737 276.6336 83.4318 15.27589379 00
| Epoch (UTC): | 25 May 2026 08:46:48 |
| Eccentricity: | 0.0001737 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.7324° |
| argument of perigee: | 276.6336° |
| revolutions per day: | 15.27589379 |
| mean anomaly at epoch: | 83.4318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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