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 63728U 26145.22705186 +.00000000 +00000-0 +27487-3 0 00009
2 63728 51.9015 97.1394 0000668 100.8251 259.2787 14.79936723 00
| Epoch (UTC): | 25 May 2026 05:26:57 |
| Eccentricity: | 0.0000668 |
| inclination: | 51.9015° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 97.1394° |
| argument of perigee: | 100.8251° |
| revolutions per day: | 14.79936723 |
| mean anomaly at epoch: | 259.2787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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