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 63917U 26145.34486256 +.00000000 +00000-0 +61442-3 0 00005
2 63917 43.0021 103.0905 0001496 255.7570 104.3115 15.27609055 02
| Epoch (UTC): | 25 May 2026 08:16:36 |
| Eccentricity: | 0.0001496 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.0905° |
| argument of perigee: | 255.7570° |
| revolutions per day: | 15.27609055 |
| mean anomaly at epoch: | 104.3115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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