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 63890U 26145.24237296 +.00000000 +00000-0 +80773-3 0 00000
2 63890 42.9980 104.0539 0001410 273.0287 87.0404 15.27588910 06
| Epoch (UTC): | 25 May 2026 05:49:01 |
| Eccentricity: | 0.0001410 |
| inclination: | 42.9980° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.0539° |
| argument of perigee: | 273.0287° |
| revolutions per day: | 15.27588910 |
| mean anomaly at epoch: | 87.0404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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