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 59512U 26145.57853374 +.00000000 +00000-0 +48445-5 0 00005
2 59512 43.0008 243.8914 0000867 270.3000 89.7752 15.27580989 05
| Epoch (UTC): | 25 May 2026 13:53:05 |
| Eccentricity: | 0.0000867 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.8914° |
| argument of perigee: | 270.3000° |
| revolutions per day: | 15.27580989 |
| mean anomaly at epoch: | 89.7752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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