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 59690U 26145.53847558 +.00000000 +00000-0 +80914-4 0 00001
2 59690 43.0032 338.2448 0001434 268.5153 91.5535 15.27577509 03
| Epoch (UTC): | 25 May 2026 12:55:24 |
| Eccentricity: | 0.0001434 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.2448° |
| argument of perigee: | 268.5153° |
| revolutions per day: | 15.27577509 |
| mean anomaly at epoch: | 91.5535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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