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 26073.61221536 +.00000000 +00000-0 +48503-3 0 00006
2 31598 97.8882 264.6838 0001598 94.6063 265.5341 14.96582605 00
| Epoch (UTC): | 14 March 2026 14:41:35 |
| Eccentricity: | 0.0001598 |
| inclination: | 97.8882° |
| perigee height: | 576 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 264.6838° |
| argument of perigee: | 94.6063° |
| revolutions per day: | 14.96582605 |
| mean anomaly at epoch: | 265.5341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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