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 63353U 26145.42201806 +.00000000 +00000-0 +21220-3 0 00004
2 63353 97.5678 121.5475 0018695 341.0110 19.0422 15.13809357 08
| Epoch (UTC): | 25 May 2026 10:07:42 |
| Eccentricity: | 0.0018695 |
| inclination: | 97.5678° |
| perigee height: | 512 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 121.5475° |
| argument of perigee: | 341.0110° |
| revolutions per day: | 15.13809357 |
| mean anomaly at epoch: | 19.0422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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