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 39267U 26032.39883323 +.00000000 +00000-0 +47034-3 0 00003
2 39267 80.9939 324.7077 0479913 349.2403 9.8803 14.75202790 00
| Epoch (UTC): | 01 February 2026 09:34:19 |
| Eccentricity: | 0.0479913 |
| inclination: | 80.9939° |
| perigee height: | 307 km |
| apogee height: | 982 km |
| right ascension of ascending node: | 324.7077° |
| argument of perigee: | 349.2403° |
| revolutions per day: | 14.75202790 |
| mean anomaly at epoch: | 9.8803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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