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 63903U 26145.35129797 +.00000000 +00000-0 +41594-3 0 00001
2 63903 43.0023 103.1461 0001569 273.1831 86.8841 15.27592869 06
| Epoch (UTC): | 25 May 2026 08:25:52 |
| Eccentricity: | 0.0001569 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.1461° |
| argument of perigee: | 273.1831° |
| revolutions per day: | 15.27592869 |
| mean anomaly at epoch: | 86.8841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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