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 26097.11959294 +.00000000 +00000-0 +57424-3 0 00009
2 39267 80.9878 252.2154 0470074 145.7162 217.5369 14.77880773 03
| Epoch (UTC): | 07 April 2026 02:52:12 |
| Eccentricity: | 0.0470074 |
| inclination: | 80.9878° |
| perigee height: | 306 km |
| apogee height: | 966 km |
| right ascension of ascending node: | 252.2154° |
| argument of perigee: | 145.7162° |
| revolutions per day: | 14.77880773 |
| mean anomaly at epoch: | 217.5369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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