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 39983U 26087.65336377 +.00000000 +00000-0 +23525-2 0 00007
2 39983 82.1425 329.9178 0045680 24.5662 5.3400 14.40940996 01
| Epoch (UTC): | 28 March 2026 15:40:50 |
| Eccentricity: | 0.0045680 |
| inclination: | 82.1425° |
| perigee height: | 723 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 329.9178° |
| argument of perigee: | 24.5662° |
| revolutions per day: | 14.40940996 |
| mean anomaly at epoch: | 5.3400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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