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 31598U 26019.24633938 +.00000000 +00000-0 +36409-3 0 00000
2 31598 97.8833 209.9010 0000932 80.1118 280.0208 14.96075345 04
| Epoch (UTC): | 19 January 2026 05:54:43 |
| Eccentricity: | 0.0000932 |
| inclination: | 97.8833° |
| perigee height: | 578 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 209.9010° |
| argument of perigee: | 80.1118° |
| revolutions per day: | 14.96075345 |
| mean anomaly at epoch: | 280.0208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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