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 26069.93058083 +.00000000 +00000-0 +41935-3 0 00001
2 39417 97.8165 31.7605 0042653 215.8183 144.0179 15.00341173 03
| Epoch (UTC): | 10 March 2026 22:20:02 |
| Eccentricity: | 0.0042653 |
| inclination: | 97.8165° |
| perigee height: | 536 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 31.7605° |
| argument of perigee: | 215.8183° |
| revolutions per day: | 15.00341173 |
| mean anomaly at epoch: | 144.0179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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