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 63086U 26145.40934219 +.00000000 +00000-0 +31690-3 0 00008
2 63086 70.0002 161.0227 0003643 264.6183 95.4560 14.98344690 06
| Epoch (UTC): | 25 May 2026 09:49:27 |
| Eccentricity: | 0.0003643 |
| inclination: | 70.0002° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 161.0227° |
| argument of perigee: | 264.6183° |
| revolutions per day: | 14.98344690 |
| mean anomaly at epoch: | 95.4560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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