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 59535U 26145.36166513 +.00000000 +00000-0 +14135-3 0 00006
2 59535 42.9974 266.6917 0000902 282.0818 77.9933 15.27585006 08
| Epoch (UTC): | 25 May 2026 08:40:47 |
| Eccentricity: | 0.0000902 |
| inclination: | 42.9974° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.6917° |
| argument of perigee: | 282.0818° |
| revolutions per day: | 15.27585006 |
| mean anomaly at epoch: | 77.9933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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