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 59504U 26145.37367317 +.00000000 +00000-0 +64756-4 0 00003
2 59504 43.0003 274.4385 0001074 278.8790 81.1940 15.27578741 01
| Epoch (UTC): | 25 May 2026 08:58:05 |
| Eccentricity: | 0.0001074 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 274.4385° |
| argument of perigee: | 278.8790° |
| revolutions per day: | 15.27578741 |
| mean anomaly at epoch: | 81.1940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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