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 63914U 26145.34874846 +.00000000 +00000-0 +55444-3 0 00003
2 63914 43.0011 103.1208 0001360 251.3261 108.7444 15.27568019 01
| Epoch (UTC): | 25 May 2026 08:22:11 |
| Eccentricity: | 0.0001360 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.1208° |
| argument of perigee: | 251.3261° |
| revolutions per day: | 15.27568019 |
| mean anomaly at epoch: | 108.7444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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