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 63960U 26145.24749068 +.00000000 +00000-0 +50835-3 0 00009
2 63960 42.9986 103.9632 0000745 260.1585 99.9182 15.27592912 02
| Epoch (UTC): | 25 May 2026 05:56:23 |
| Eccentricity: | 0.0000745 |
| inclination: | 42.9986° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.9632° |
| argument of perigee: | 260.1585° |
| revolutions per day: | 15.27592912 |
| mean anomaly at epoch: | 99.9182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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