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 16631U 26140.22606353 +.00000000 +00000-0 +32764-3 0 00005
2 16631 63.2928 107.6888 0757004 111.9699 256.3523 13.91741896 01
| Epoch (UTC): | 20 May 2026 05:25:31 |
| Eccentricity: | 0.0757004 |
| inclination: | 63.2928° |
| perigee height: | 370 km |
| apogee height: | 1475 km |
| right ascension of ascending node: | 107.6888° |
| argument of perigee: | 111.9699° |
| revolutions per day: | 13.91741896 |
| mean anomaly at epoch: | 256.3523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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