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 62143U 26145.52102234 +.00000000 +00000-0 +38499-3 0 00002
2 62143 42.9989 87.3798 0000917 276.4571 83.6176 15.27585997 09
| Epoch (UTC): | 25 May 2026 12:30:16 |
| Eccentricity: | 0.0000917 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.3798° |
| argument of perigee: | 276.4571° |
| revolutions per day: | 15.27585997 |
| mean anomaly at epoch: | 83.6176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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