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 26106.59869580 +.00000000 +00000-0 +61595-3 0 00000
2 31702 63.3098 61.4964 0498175 42.8747 321.0066 14.52965418 03
| Epoch (UTC): | 16 April 2026 14:22:07 |
| Eccentricity: | 0.0498175 |
| inclination: | 63.3098° |
| perigee height: | 363 km |
| apogee height: | 1069 km |
| right ascension of ascending node: | 61.4964° |
| argument of perigee: | 42.8747° |
| revolutions per day: | 14.52965418 |
| mean anomaly at epoch: | 321.0066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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