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 26040.91444794 +.00000000 +00000-0 +33055-3 0 00002
2 31598 97.8858 231.7290 0000844 82.1148 278.0169 14.96311544 08
| Epoch (UTC): | 09 February 2026 21:56:48 |
| Eccentricity: | 0.0000844 |
| inclination: | 97.8858° |
| perigee height: | 578 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 231.7290° |
| argument of perigee: | 82.1148° |
| revolutions per day: | 14.96311544 |
| mean anomaly at epoch: | 278.0169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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