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 26114.19266696 +.00000000 +00000-0 +17580-3 0 00002
2 31598 97.8870 305.5995 0001216 101.0317 259.1041 14.96827855 03
| Epoch (UTC): | 24 April 2026 04:37:26 |
| Eccentricity: | 0.0001216 |
| inclination: | 97.8870° |
| perigee height: | 576 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 305.5995° |
| argument of perigee: | 101.0317° |
| revolutions per day: | 14.96827855 |
| mean anomaly at epoch: | 259.1041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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