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 26072.94361116 +.00000000 +00000-0 +42908-3 0 00003
2 31598 97.8882 264.0096 0001578 95.4766 264.6635 14.96574619 09
| Epoch (UTC): | 13 March 2026 22:38:48 |
| Eccentricity: | 0.0001578 |
| inclination: | 97.8882° |
| perigee height: | 576 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 264.0096° |
| argument of perigee: | 95.4766° |
| revolutions per day: | 14.96574619 |
| mean anomaly at epoch: | 264.6635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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