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 63323U 26145.49125810 +.00000000 +00000-0 +93090-3 0 00002
2 63323 42.9994 317.0842 0003374 282.2047 77.8426 15.27604001 03
| Epoch (UTC): | 25 May 2026 11:47:24 |
| Eccentricity: | 0.0003374 |
| inclination: | 42.9994° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 317.0842° |
| argument of perigee: | 282.2047° |
| revolutions per day: | 15.27604001 |
| mean anomaly at epoch: | 77.8426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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