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 59640U 26145.46868139 +.00000000 +00000-0 +49791-5 0 00005
2 59640 43.0008 66.2569 0000986 262.7291 97.3448 15.27572646 07
| Epoch (UTC): | 25 May 2026 11:14:54 |
| Eccentricity: | 0.0000986 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.2569° |
| argument of perigee: | 262.7291° |
| revolutions per day: | 15.27572646 |
| mean anomaly at epoch: | 97.3448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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