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 26072.23927809 +.00000000 +00000-0 +66711-3 0 00007
2 31702 63.3109 167.8403 0499988 42.2916 321.5602 14.51678034 05
| Epoch (UTC): | 13 March 2026 05:44:33 |
| Eccentricity: | 0.0499988 |
| inclination: | 63.3109° |
| perigee height: | 365 km |
| apogee height: | 1075 km |
| right ascension of ascending node: | 167.8403° |
| argument of perigee: | 42.2916° |
| revolutions per day: | 14.51678034 |
| mean anomaly at epoch: | 321.5602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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