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 26106.77232461 +.00000000 +00000-0 +10262-3 0 00000
2 31598 97.8877 298.1180 0001298 85.9326 274.2043 14.96803552 01
| Epoch (UTC): | 16 April 2026 18:32:08 |
| Eccentricity: | 0.0001298 |
| inclination: | 97.8877° |
| perigee height: | 576 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 298.1180° |
| argument of perigee: | 85.9326° |
| revolutions per day: | 14.96803552 |
| mean anomaly at epoch: | 274.2043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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