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 59572U 26145.13083917 +.00000000 +00000-0 +72560-4 0 00005
2 59572 43.0047 290.3325 0001077 271.3548 88.7180 15.27571562 00
| Epoch (UTC): | 25 May 2026 03:08:24 |
| Eccentricity: | 0.0001077 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 290.3325° |
| argument of perigee: | 271.3548° |
| revolutions per day: | 15.27571562 |
| mean anomaly at epoch: | 88.7180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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