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 63132U 26145.38836648 +.00000000 +00000-0 +12085-2 0 00000
2 63132 42.9982 148.5121 0000770 261.4393 98.6387 15.70870478 03
| Epoch (UTC): | 25 May 2026 09:19:14 |
| Eccentricity: | 0.0000770 |
| inclination: | 42.9982° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 148.5121° |
| argument of perigee: | 261.4393° |
| revolutions per day: | 15.70870478 |
| mean anomaly at epoch: | 98.6387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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