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 59309U 26145.46940209 +.00000000 +00000-0 +10539-4 0 00003
2 59309 43.0026 153.9131 0001073 275.2014 84.8715 15.27577471 07
| Epoch (UTC): | 25 May 2026 11:15:56 |
| Eccentricity: | 0.0001073 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.9131° |
| argument of perigee: | 275.2014° |
| revolutions per day: | 15.27577471 |
| mean anomaly at epoch: | 84.8715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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