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 63239U 26145.46405748 +.00000000 +00000-0 +53647-3 0 00000
2 63239 97.3970 40.7471 0005114 205.0862 155.0131 15.30801513 00
| Epoch (UTC): | 25 May 2026 11:08:14 |
| Eccentricity: | 0.0005114 |
| inclination: | 97.3970° |
| perigee height: | 470 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 40.7471° |
| argument of perigee: | 205.0862° |
| revolutions per day: | 15.30801513 |
| mean anomaly at epoch: | 155.0131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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