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 26075.95892273 +.00000000 +00000-0 +58828-3 0 00005
2 31702 63.3112 156.3394 0499789 42.3558 321.4994 14.51801765 05
| Epoch (UTC): | 16 March 2026 23:00:50 |
| Eccentricity: | 0.0499789 |
| inclination: | 63.3112° |
| perigee height: | 365 km |
| apogee height: | 1075 km |
| right ascension of ascending node: | 156.3394° |
| argument of perigee: | 42.3558° |
| revolutions per day: | 14.51801765 |
| mean anomaly at epoch: | 321.4994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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