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 59748U 26144.95682154 +.00000000 +00000-0 +21235-4 0 00000
2 59748 43.0023 112.8254 0001018 268.0999 91.9736 15.27576427 04
| Epoch (UTC): | 24 May 2026 22:57:49 |
| Eccentricity: | 0.0001018 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 112.8254° |
| argument of perigee: | 268.0999° |
| revolutions per day: | 15.27576427 |
| mean anomaly at epoch: | 91.9736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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