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 63143U 26145.35650414 +.00000000 +00000-0 +16739-2 0 00004
2 63143 43.0036 148.2472 0002147 253.9539 106.1093 15.70886830 09
| Epoch (UTC): | 25 May 2026 08:33:21 |
| Eccentricity: | 0.0002147 |
| inclination: | 43.0036° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 148.2472° |
| argument of perigee: | 253.9539° |
| revolutions per day: | 15.70886830 |
| mean anomaly at epoch: | 106.1093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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