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 26021.25280373 +.00000000 +00000-0 +10225-2 0 00002
2 31598 97.8836 211.9218 0000965 88.2834 271.8497 14.96113161 07
| Epoch (UTC): | 21 January 2026 06:04:02 |
| Eccentricity: | 0.0000965 |
| inclination: | 97.8836° |
| perigee height: | 578 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 211.9218° |
| argument of perigee: | 88.2834° |
| revolutions per day: | 14.96113161 |
| mean anomaly at epoch: | 271.8497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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