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 26017.30672455 +.00000000 +00000-0 +24948-3 0 00007
2 31598 97.8837 207.9477 0001017 76.0152 284.1182 14.96062693 08
| Epoch (UTC): | 17 January 2026 07:21:41 |
| Eccentricity: | 0.0001017 |
| inclination: | 97.8837° |
| perigee height: | 578 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 207.9477° |
| argument of perigee: | 76.0152° |
| revolutions per day: | 14.96062693 |
| mean anomaly at epoch: | 284.1182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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