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 26040.24572366 +.00000000 +00000-0 +30896-3 0 00005
2 31598 97.8857 231.0552 0000859 79.5255 280.6063 14.96305708 03
| Epoch (UTC): | 09 February 2026 05:53:50 |
| Eccentricity: | 0.0000859 |
| inclination: | 97.8857° |
| perigee height: | 578 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 231.0552° |
| argument of perigee: | 79.5255° |
| revolutions per day: | 14.96305708 |
| mean anomaly at epoch: | 280.6063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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