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 39417U 26075.13256441 +.00000000 +00000-0 +27393-3 0 00000
2 39417 97.8156 36.9877 0043283 198.5806 161.3839 15.00390975 09
| Epoch (UTC): | 16 March 2026 03:10:53 |
| Eccentricity: | 0.0043283 |
| inclination: | 97.8156° |
| perigee height: | 536 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 36.9877° |
| argument of perigee: | 198.5806° |
| revolutions per day: | 15.00390975 |
| mean anomaly at epoch: | 161.3839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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