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 26041.51629818 +.00000000 +00000-0 +32439-3 0 00006
2 31598 97.8857 232.3353 0000850 84.2414 275.8904 14.96315811 03
| Epoch (UTC): | 10 February 2026 12:23:28 |
| Eccentricity: | 0.0000850 |
| inclination: | 97.8857° |
| perigee height: | 578 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 232.3353° |
| argument of perigee: | 84.2414° |
| revolutions per day: | 14.96315811 |
| mean anomaly at epoch: | 275.8904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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