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 63908U 26145.25393140 +.00000000 +00000-0 +11151-2 0 00005
2 63908 42.9991 104.1399 0001143 249.0711 111.0018 15.27571314 00
| Epoch (UTC): | 25 May 2026 06:05:39 |
| Eccentricity: | 0.0001143 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.1399° |
| argument of perigee: | 249.0711° |
| revolutions per day: | 15.27571314 |
| mean anomaly at epoch: | 111.0018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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