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 31702U 26073.61696328 +.00000000 +00000-0 +91057-3 0 00000
2 31702 63.3110 163.5810 0499841 42.3190 321.5337 14.51731954 01
| Epoch (UTC): | 14 March 2026 14:48:25 |
| Eccentricity: | 0.0499841 |
| inclination: | 63.3110° |
| perigee height: | 365 km |
| apogee height: | 1075 km |
| right ascension of ascending node: | 163.5810° |
| argument of perigee: | 42.3190° |
| revolutions per day: | 14.51731954 |
| mean anomaly at epoch: | 321.5337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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