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 26146.26148076 +.00000000 +00000-0 +47457-3 0 00003
2 16631 63.2930 90.6553 0756506 112.0862 256.2247 13.91818162 07
| Epoch (UTC): | 26 May 2026 06:16:31 |
| Eccentricity: | 0.0756506 |
| inclination: | 63.2930° |
| perigee height: | 370 km |
| apogee height: | 1475 km |
| right ascension of ascending node: | 90.6553° |
| argument of perigee: | 112.0862° |
| revolutions per day: | 13.91818162 |
| mean anomaly at epoch: | 256.2247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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