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 63139U 26145.37774201 +.00000000 +00000-0 +13040-2 0 00004
2 63139 42.9986 148.4240 0001597 247.1466 112.9233 15.70878024 00
| Epoch (UTC): | 25 May 2026 09:03:56 |
| Eccentricity: | 0.0001597 |
| inclination: | 42.9986° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 148.4240° |
| argument of perigee: | 247.1466° |
| revolutions per day: | 15.70878024 |
| mean anomaly at epoch: | 112.9233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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