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 39166U 26144.74992255 +.00000000 +00000-0 +00000-0 0 00008
2 39166 54.5230 269.9280 0141731 50.9138 310.3242 2.00563616 09
| Epoch (UTC): | 24 May 2026 17:59:53 |
| Eccentricity: | 0.0141731 |
| inclination: | 54.5230° |
| perigee height: | 19806 km |
| apogee height: | 20559 km |
| right ascension of ascending node: | 269.9280° |
| argument of perigee: | 50.9138° |
| revolutions per day: | 2.00563616 |
| mean anomaly at epoch: | 310.3242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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