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 26041.36830220 +.00000000 +00000-0 +42047-3 0 00007
2 16631 63.2943 26.3203 0769392 110.0291 258.5233 13.89824191 06
| Epoch (UTC): | 10 February 2026 08:50:21 |
| Eccentricity: | 0.0769392 |
| inclination: | 63.2943° |
| perigee height: | 367 km |
| apogee height: | 1491 km |
| right ascension of ascending node: | 26.3203° |
| argument of perigee: | 110.0291° |
| revolutions per day: | 13.89824191 |
| mean anomaly at epoch: | 258.5233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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