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 26032.48834750 +.00000000 +00000-0 +27696-3 0 00004
2 31598 97.8858 223.2397 0001443 79.8277 280.3106 14.96241031 04
| Epoch (UTC): | 01 February 2026 11:43:13 |
| Eccentricity: | 0.0001443 |
| inclination: | 97.8858° |
| perigee height: | 578 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 223.2397° |
| argument of perigee: | 79.8277° |
| revolutions per day: | 14.96241031 |
| mean anomaly at epoch: | 280.3106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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