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 63232U 26145.28230063 +.00000000 +00000-0 +23544-3 0 00002
2 63232 97.3979 38.6060 0004522 214.7126 145.3817 15.23638736 04
| Epoch (UTC): | 25 May 2026 06:46:30 |
| Eccentricity: | 0.0004522 |
| inclination: | 97.3979° |
| perigee height: | 492 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 38.6060° |
| argument of perigee: | 214.7126° |
| revolutions per day: | 15.23638736 |
| mean anomaly at epoch: | 145.3817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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