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 62600U 26145.60405697 +.00000000 +00000-0 +56008-3 0 00004
2 62600 43.0018 203.8831 0001363 272.1782 87.8913 15.27593041 02
| Epoch (UTC): | 25 May 2026 14:29:50 |
| Eccentricity: | 0.0001363 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 203.8831° |
| argument of perigee: | 272.1782° |
| revolutions per day: | 15.27593041 |
| mean anomaly at epoch: | 87.8913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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