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 63975U 26145.24926877 +.00000000 +00000-0 +24410-3 0 00000
2 63975 42.9997 100.5080 0001392 258.9962 101.0733 15.27556359 05
| Epoch (UTC): | 25 May 2026 05:58:56 |
| Eccentricity: | 0.0001392 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.5080° |
| argument of perigee: | 258.9962° |
| revolutions per day: | 15.27556359 |
| mean anomaly at epoch: | 101.0733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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