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 62286U 26145.47458855 +.00000000 +00000-0 +68229-3 0 00001
2 62286 43.0003 142.8516 0001662 272.5754 87.4907 15.27597845 08
| Epoch (UTC): | 25 May 2026 11:23:24 |
| Eccentricity: | 0.0001662 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 142.8516° |
| argument of perigee: | 272.5754° |
| revolutions per day: | 15.27597845 |
| mean anomaly at epoch: | 87.4907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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