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 26075.86616470 +.00000000 +00000-0 +26382-3 0 00009
2 39417 97.8156 37.7248 0043381 196.1948 163.7891 15.00396719 06
| Epoch (UTC): | 16 March 2026 20:47:16 |
| Eccentricity: | 0.0043381 |
| inclination: | 97.8156° |
| perigee height: | 536 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 37.7248° |
| argument of perigee: | 196.1948° |
| revolutions per day: | 15.00396719 |
| mean anomaly at epoch: | 163.7891° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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