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 59316U 26145.49541689 +.00000000 +00000-0 +18210-4 0 00007
2 59316 43.0028 161.0239 0001220 283.1469 76.9246 15.27577107 09
| Epoch (UTC): | 25 May 2026 11:53:24 |
| Eccentricity: | 0.0001220 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 161.0239° |
| argument of perigee: | 283.1469° |
| revolutions per day: | 15.27577107 |
| mean anomaly at epoch: | 76.9246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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