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 26106.97287580 +.00000000 +00000-0 +10614-3 0 00005
2 31598 97.8877 298.3203 0001284 86.0970 274.0398 14.96804197 08
| Epoch (UTC): | 16 April 2026 23:20:56 |
| Eccentricity: | 0.0001284 |
| inclination: | 97.8877° |
| perigee height: | 576 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 298.3203° |
| argument of perigee: | 86.0970° |
| revolutions per day: | 14.96804197 |
| mean anomaly at epoch: | 274.0398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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