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 26065.35019389 +.00000000 +00000-0 +60797-3 0 00005
2 31702 63.3114 189.1360 0500167 42.2005 321.6459 14.51444243 05
| Epoch (UTC): | 06 March 2026 08:24:16 |
| Eccentricity: | 0.0500167 |
| inclination: | 63.3114° |
| perigee height: | 366 km |
| apogee height: | 1076 km |
| right ascension of ascending node: | 189.1360° |
| argument of perigee: | 42.2005° |
| revolutions per day: | 14.51444243 |
| mean anomaly at epoch: | 321.6459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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