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 60436U 26145.50405343 +.00000000 +00000-0 +23635-4 0 00007
2 60436 53.1604 219.3529 0000949 89.3473 270.7638 15.34387020 03
| Epoch (UTC): | 25 May 2026 12:05:50 |
| Eccentricity: | 0.0000949 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.3529° |
| argument of perigee: | 89.3473° |
| revolutions per day: | 15.34387020 |
| mean anomaly at epoch: | 270.7638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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