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 63738U 26145.17442676 +.00000000 +00000-0 +19889-3 0 00003
2 63738 51.9025 114.9180 0000638 65.8335 294.2694 14.79933961 00
| Epoch (UTC): | 25 May 2026 04:11:10 |
| Eccentricity: | 0.0000638 |
| inclination: | 51.9025° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 114.9180° |
| argument of perigee: | 65.8335° |
| revolutions per day: | 14.79933961 |
| mean anomaly at epoch: | 294.2694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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