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 63907U 26145.01023021 +.00000000 +00000-0 +77300-3 0 00005
2 63907 43.0000 104.8841 0001458 271.0598 89.0087 15.27598513 08
| Epoch (UTC): | 25 May 2026 00:14:43 |
| Eccentricity: | 0.0001458 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.8841° |
| argument of perigee: | 271.0598° |
| revolutions per day: | 15.27598513 |
| mean anomaly at epoch: | 89.0087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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