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 26068.53075061 +.00000000 +00000-0 +37891-3 0 00009
2 31598 97.8871 259.5611 0001235 100.7828 259.3532 14.96532459 01
| Epoch (UTC): | 09 March 2026 12:44:16 |
| Eccentricity: | 0.0001235 |
| inclination: | 97.8871° |
| perigee height: | 577 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 259.5611° |
| argument of perigee: | 100.7828° |
| revolutions per day: | 14.96532459 |
| mean anomaly at epoch: | 259.3532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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