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 63685U 26145.54512580 +.00000000 +00000-0 +84353-3 0 00005
2 63685 42.9995 316.9011 0001313 248.0478 112.0234 15.27587597 09
| Epoch (UTC): | 25 May 2026 13:04:58 |
| Eccentricity: | 0.0001313 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.9011° |
| argument of perigee: | 248.0478° |
| revolutions per day: | 15.27587597 |
| mean anomaly at epoch: | 112.0234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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