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 63742U 26145.17569566 +.00000000 +00000-0 +26387-3 0 00007
2 63742 51.9017 113.4169 0002980 82.6742 277.4558 14.76578045 05
| Epoch (UTC): | 25 May 2026 04:13:00 |
| Eccentricity: | 0.0002980 |
| inclination: | 51.9017° |
| perigee height: | 638 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 113.4169° |
| argument of perigee: | 82.6742° |
| revolutions per day: | 14.76578045 |
| mean anomaly at epoch: | 277.4558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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