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 63910U 26145.37699878 +.00000000 +00000-0 +24228-3 0 00008
2 63910 42.9983 103.3424 0001212 269.9945 90.0767 15.27582950 06
| Epoch (UTC): | 25 May 2026 09:02:52 |
| Eccentricity: | 0.0001212 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.3424° |
| argument of perigee: | 269.9945° |
| revolutions per day: | 15.27582950 |
| mean anomaly at epoch: | 90.0767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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