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 59741U 26145.36198910 +.00000000 +00000-0 +64110-4 0 00000
2 59741 43.0037 110.7070 0001368 285.6479 74.4221 15.27580613 08
| Epoch (UTC): | 25 May 2026 08:41:15 |
| Eccentricity: | 0.0001368 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.7070° |
| argument of perigee: | 285.6479° |
| revolutions per day: | 15.27580613 |
| mean anomaly at epoch: | 74.4221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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