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 59314U 26145.46973919 +.00000000 +00000-0 +18656-4 0 00001
2 59314 43.0036 149.5876 0001439 283.4419 76.6272 15.27575701 08
| Epoch (UTC): | 25 May 2026 11:16:25 |
| Eccentricity: | 0.0001439 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 149.5876° |
| argument of perigee: | 283.4419° |
| revolutions per day: | 15.27575701 |
| mean anomaly at epoch: | 76.6272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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