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 63635U 26145.41616397 +.00000000 +00000-0 +81491-3 0 00007
2 63635 42.9995 291.6941 0001809 268.1112 91.9533 15.27596018 08
| Epoch (UTC): | 25 May 2026 09:59:16 |
| Eccentricity: | 0.0001809 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.6941° |
| argument of perigee: | 268.1112° |
| revolutions per day: | 15.27596018 |
| mean anomaly at epoch: | 91.9533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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