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 59304U 26145.32497703 +.00000000 +00000-0 -61763-4 0 00005
2 59304 43.0019 151.0818 0000999 261.0264 99.0475 15.27589083 04
| Epoch (UTC): | 25 May 2026 07:47:58 |
| Eccentricity: | 0.0000999 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 151.0818° |
| argument of perigee: | 261.0264° |
| revolutions per day: | 15.27589083 |
| mean anomaly at epoch: | 99.0475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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