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 63906U 26145.34101948 +.00000000 +00000-0 +94426-3 0 00003
2 63906 43.0016 103.0691 0001567 320.1707 39.9030 15.27603998 03
| Epoch (UTC): | 25 May 2026 08:11:04 |
| Eccentricity: | 0.0001567 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.0691° |
| argument of perigee: | 320.1707° |
| revolutions per day: | 15.27603998 |
| mean anomaly at epoch: | 39.9030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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